This document discusses analysis of ground-penetrating radar (GPR) data from single-channel and multi-channel surveys. It finds that channel 4 of the multi-channel GPR system produces low amplitudes, making air-wave picking imprecise. Placement of antenna cables on the center vs. side of the sled also affects air-wave arrival times. Semblance analysis, used to pick ground waves, breaks down under non-linear waves, use of selected traces only, and gained data. The source of uncertainty in GPR data includes skipped traces and temporal drift of time-zero corrections between measurements.
This technical note discusses synchronization of tracking antennas for a satellite detection system using sky-scanning techniques. It proposes synchronizing antenna sweeps between transmitter and receiver sites up to 1000 miles apart to within 1 degree. Potential methods include directly connecting sites, synchronizing each to a common time source like WWV, or using precision local time generators synchronized to WWV. Antenna sweep rates of 6, 9, or 12 degrees per second are recommended to simplify synchronization. Synchronization is deemed entirely practical through use of stable local oscillators synchronized to WWV time signals.
The document describes the development of an experimental test rig for testing a dual fuel and diesel engine. Key components of the test rig include an L-shaped channel frame, Bakelite boards for mounting instrumentation, and panels for controls and loads. Instruments such as a voltmeter, ammeter, tachometer, temperature indicators, and fuel flow meters were installed to measure voltage, current, RPM, temperature, and fuel consumption. The test rig was designed to provide measurements needed to analyze parameters like power, speed, temperature, and fuel efficiency of the engine.
An independent flush air data system (FADS) was designed and installed on a Boeing B707 aircraft to provide real-time air data for flight testing without interfering with the aircraft. The FADS used pressures measured by sensors on the nose radome to compute air data parameters like angle of attack and sideslip through a mathematical model. The model was calibrated and computations were performed in real-time at a rate of 2.5 Hz during flight tests to generate air data for simulator development. Post-flight processing recomputed the air data at 50 Hz for further analysis.
The document discusses thrust vector control systems which redirect engine thrust to control aircraft attitude. It focuses on the jet deflection method, where small airfoils located at the nozzle exit plane cause thrust to be vectored. The goals are to analyze this system using CFD. NACA 0012 airfoils are selected due to symmetrical shape and lift characteristics. CFD will be used to simulate fluid flow and predict system performance before manufacturing. Key benefits of CFD include insight into designs, ability to test variants efficiently, and compressing development cycles.
The performance of a hydraulic turbine is influenced by the characteristics of the water column feeding the turbine:
water inertia
water compressibility
pipe wall elasticity in the penstock
The effect of water inertia is to cause changes in turbine flow to lag behind changes in turbine gate opening
The effect of elasticity is to cause traveling waves of pressure and flow in the pipe - a phenomenon referred to as water hammer
typically, the speed of propagation of such waves is about 1200 meters/sec
traveling wave model required only if penstock is very long
Hydraulic Turbines and Governing Systems
Hydraulic turbine transfer function
special characteristics of hydraulic turbines
nonlinear hydraulic turbine model
governors for hydraulic turbines
tuning of speed governors
Steam Turbines and Governing Systems
steam turbine configurations
steam turbine models
steam turbine controls
Gas Turbines and Governing Systems
simple-cycle configuration
combined-cycle configuration
A Novel Multi Port Dc/Dc Converter Topology Using Zero Voltage Switching For...IJMER
This paper proposes a novel four-port DC/DC converter topology that can interface two renewable energy sources, a bidirectional battery storage port, and an isolated load port. The topology is derived from a traditional half-bridge converter with the addition of two switches and diodes. All four main switches can achieve zero-voltage switching, reducing switching losses. MATLAB simulations and experimental results validate the circuit operation and regulation of the multiple power ports via independent duty cycle control. The proposed topology is suitable for applications integrating hybrid photovoltaic and wind energy systems with battery storage.
This technical note discusses synchronization of tracking antennas for a satellite detection system using sky-scanning techniques. It proposes synchronizing antenna sweeps between transmitter and receiver sites up to 1000 miles apart to within 1 degree. Potential methods include directly connecting sites, synchronizing each to a common time source like WWV, or using precision local time generators synchronized to WWV. Antenna sweep rates of 6, 9, or 12 degrees per second are recommended to simplify synchronization. Synchronization is deemed entirely practical through use of stable local oscillators synchronized to WWV time signals.
The document describes the development of an experimental test rig for testing a dual fuel and diesel engine. Key components of the test rig include an L-shaped channel frame, Bakelite boards for mounting instrumentation, and panels for controls and loads. Instruments such as a voltmeter, ammeter, tachometer, temperature indicators, and fuel flow meters were installed to measure voltage, current, RPM, temperature, and fuel consumption. The test rig was designed to provide measurements needed to analyze parameters like power, speed, temperature, and fuel efficiency of the engine.
An independent flush air data system (FADS) was designed and installed on a Boeing B707 aircraft to provide real-time air data for flight testing without interfering with the aircraft. The FADS used pressures measured by sensors on the nose radome to compute air data parameters like angle of attack and sideslip through a mathematical model. The model was calibrated and computations were performed in real-time at a rate of 2.5 Hz during flight tests to generate air data for simulator development. Post-flight processing recomputed the air data at 50 Hz for further analysis.
The document discusses thrust vector control systems which redirect engine thrust to control aircraft attitude. It focuses on the jet deflection method, where small airfoils located at the nozzle exit plane cause thrust to be vectored. The goals are to analyze this system using CFD. NACA 0012 airfoils are selected due to symmetrical shape and lift characteristics. CFD will be used to simulate fluid flow and predict system performance before manufacturing. Key benefits of CFD include insight into designs, ability to test variants efficiently, and compressing development cycles.
The performance of a hydraulic turbine is influenced by the characteristics of the water column feeding the turbine:
water inertia
water compressibility
pipe wall elasticity in the penstock
The effect of water inertia is to cause changes in turbine flow to lag behind changes in turbine gate opening
The effect of elasticity is to cause traveling waves of pressure and flow in the pipe - a phenomenon referred to as water hammer
typically, the speed of propagation of such waves is about 1200 meters/sec
traveling wave model required only if penstock is very long
Hydraulic Turbines and Governing Systems
Hydraulic turbine transfer function
special characteristics of hydraulic turbines
nonlinear hydraulic turbine model
governors for hydraulic turbines
tuning of speed governors
Steam Turbines and Governing Systems
steam turbine configurations
steam turbine models
steam turbine controls
Gas Turbines and Governing Systems
simple-cycle configuration
combined-cycle configuration
A Novel Multi Port Dc/Dc Converter Topology Using Zero Voltage Switching For...IJMER
This paper proposes a novel four-port DC/DC converter topology that can interface two renewable energy sources, a bidirectional battery storage port, and an isolated load port. The topology is derived from a traditional half-bridge converter with the addition of two switches and diodes. All four main switches can achieve zero-voltage switching, reducing switching losses. MATLAB simulations and experimental results validate the circuit operation and regulation of the multiple power ports via independent duty cycle control. The proposed topology is suitable for applications integrating hybrid photovoltaic and wind energy systems with battery storage.
Nasa tech briefs ksk 11495, simplified model of duct flowJulio Banks
This document provides technical details on a simplified model for analyzing transient duct flow, including:
- A one-dimensional model is developed using a perturbation of duct exit area to account for friction loss and relate transient to quasi-steady duct velocity with a differential equation.
- Computer programs are included that calculate duct exit momentum through an iterative momentum balance between inlet and outlet, incorporating engine shock loss and additional duct combustion.
- Validation shows the model correlates well with single engine helium and steam test data over a range of chamber pressures.
- Application to full-scale conditions indicates maximum air flow is less than actual Space Shuttle levels, suggesting helium flow alone cannot replicate critical conditions.
P&w tables of compressible flow functionsJulio Banks
Compressible-flow Mach Functionas
Page 5 - Nomenclature
Pages 6 & 7 - Mach Functions
Recommendaitons: Used Equations on Pp. 6 & 7 to
generate any of the results from the table as functions
of specific heat ration, Gamma = Cp/Cv.
Enjoy it as one would enjoy their favorite music.
The document describes default test templates in the Raptor HH device for testing various electrical equipment. It includes:
1. Templates for circuit breaker testing, overcurrent relay testing, current transformer testing, Rogowski coil testing, AC resistance measurement, ground grid testing, and CT burden testing.
2. Templates for voltage transformer testing, VT burden testing, and short-circuited potential transformer testing.
3. A template for measuring potential transformer ratios.
The templates allow automatic or semi-automatic testing of this equipment by selecting the appropriate template and configuring test parameters.
Study and Development of an Energy Saving Mechanical SystemIDES Editor
A new energy-saving mechanical system with
automatically controlled air valves has been proposed by
investigator and the preliminary model setup has been tested.
The testing results indicated the proper function of this
energy-saving mechanical system. This mechanical system
model has been simulated and analyzed by the computational
aided engineering solution. The major advantages of this
mechanical system include: simple and compact in design,
higher efficiency in mechanical functioning, quiet in
manufacturing operation, less energy losses due to less
frictional forces in this free piston-cylinder setup, selfadjustable
in operational parameter to improve the system
performance, and etc.
The document describes a series of use cases (UC-832, UC-833) for calibrating and running hydrological models in a common service. It involves downloading data, creating local models, calibrating models, performing simulations, and exploring results. Key steps include selecting areas of interest, adding observation stations, calibrating models using station data, running simulations with climate scenarios, and viewing output time series.
This document provides instructions for an experiment involving the regulation of a three-phase salient pole alternator. It includes the objectives, list of experiments, theory, circuit diagram, nameplate details, observations, calculations, precautions and procedures for conducting the slip test experiment to determine the alternator's regulation by varying the load and measuring voltages and currents. The goal is to calculate the direct axis and quadrature axis reactances and plot the regulation curves at varying power factors to understand the alternator's performance characteristics.
The document provides instructions for experiments to be conducted in the Control Systems Lab course at BTL Institute of Technology and Management in Bangalore, India. It lists 11 experiments involving designing and analyzing compensating networks, studying controller performance, and using MATLAB/SCILAB for simulations. The experiments are divided into two cycles, with the first cycle focusing on hardware implementations and the second on software simulations. Specific procedures are given for designing and characterizing lead and lag compensators.
ENHANCED DATA DRIVEN MODE-FREE ADAPTIVE YAW CONTROL OF UAV HELICOPTERijics
An enhanced data driven model-free adaptive yaw control tracking control scheme is proposed for the yaw
channel of an unmanned-aerial-vehicle (UAV) helicopter which is non-affine in the control input in this paper. Through dynamic linearization and observer techniques, the proposed control algorithm is only based on the pseudo-partial derivative (PPD) parameter estimation derived online from the I/O data of the yaw channel of an UAV helicopter, and Lyapunov-based stability analysis is utilized to prove all signals of
close-loop control system are bounded. Compared with the traditional model free adaptive control
(MFAC), the proposed enhanced MFAC algorithm can make the close-loop control system with stronger robustness and better anti-jamming ability. Finally, simulation results of the UAV yaw channel are offered to demonstrate the effectiveness of the proposed novel control technique.
A Simplified Speed Control Of Induction Motor based on a Low Cost FPGA IJECEIAES
This paper investigates the development of a simplified speed control of induction motor based on indirect field oriented control (FOC). An original PI-P controller is designed to obtain good performances for speed tracking. Controller coefficients are carried out with analytic approach. The algorithm is implemented using a low cost Field Programmable Gate Array (FPGA). The implementation is followed by an efficient design methodology that offers considerable design advantages. The main advantage is the design of reusable and reconfigurable hardware modules for the control of electrical systems. Experimental results carried on a prototyping platform are given to illustrate the efficiency and the benefits of the proposed approach.
Turbofan Engine Modelling and Control Design using Linear Quadratic Regulator...theijes
There are many applications in which gas turbine engine is used today, including aircraft propulsion for both commercial and military purposes, and power generation and in all these Control systems technology has played a fundamental role in enhancing performance. Modelling plays a significant role in the development of the entire engine system performance. This paper investigated Linear Quadratic Regulator (LQR) model-based control method to obtain estimates of performance parameters. The main control variable selected is the fuel flow to control the rotational speed of high-pressure spool speed of the turbofan engine. Firstly a suitable mathematical model of the engine is developed in MATLAB Simulink environment with both the intercomponent volume and the constant mass flow methods used. Equations of the mass flow rate and the torque balance are incorporated in the steady state and dynamic state of the thermodynamic engine model. This represents the engine model by a set of first-order differential and algebraic equations and a linearized model is extracted for the analysis and design of a controller by LQR. It is demonstrated that LQR based controllers can perform better than conventional PID controllers. The settling time, rise time and maximum overshoot for LQR based controller are all less than those for PID based controller. The input also changes more accurately for LQR than the PID controller compared.
Mobile instrumentation and_data_processing_system_for_testinglkantwani
This document describes a mobile instrumentation and data processing system for testing agricultural field machinery. The system collects data from sensors mounted on tractors and implements during field tests, including three-point hitch forces, PTO torque and speed, forward speed, wheel slip, fuel flow, and depth of work. Data is transmitted via radio telemetry to a vehicle where it is recorded and processed. The system provides processed data in the field to modify tests and identify performance issues. Field tests examined the effects of different soil contact pressures on soil and crops. The system allows efficient testing at remote field sites with real-time data analysis.
This document provides an overview of global positioning systems and flight management systems used in aircraft. It defines key terms and describes the components and functions of GPS, WAAS, INS, barometric altimeters, and how they integrate with an aircraft's flight management system. It explains how GPS and WAAS provide lateral and vertical navigation guidance for different types of instrument approaches, including LNAV, LNAV+V, LNAV/VNAV, LP, and LPV approaches. It also covers requirements, limitations, and safety aspects of using GPS and WAAS for navigation.
Automated Testing of C-Band Rotary Field Ferrite Phase ShifterIJERA Editor
This paper presents the methodology for an automatic test procedure based on LabVIEW for RF characterisation of C- band rotary field phase shifter. Using this software, the characteristics of the phase shifter intended for phased array application viz. differential phase shift, insertion loss, return loss, rms phase error, insertion phase are measured systematically and displayed graphically in user friendly format.
This document presents SEA, an experimental testing environment for electrohydraulic actuators. SEA allows for precise measurement of important actuator variables to enable comprehensive static and dynamic characterization. It includes a hydraulic pump and pipelines, configurable loads, an instrumented manifold for measurements, and a DAQ system. Experimental results from characterizing an aerospace actuator using SEA are provided, including static calibration, transient response testing showing high pressure and flow demands, and system identification to develop an input-output mathematical model. SEA provides an effective environment for full experimental characterization of electrohydraulic actuators.
The document proposes a switching strategy for space vector modulated current link inverters connected to the power grid. It discusses pulse width modulation techniques and space vector pulse width modulation. The proposed strategy uses symmetrical cell time switching sequences to realize the six current vectors and minimize harmonics. Analytical calculations and experimental results show the strategy provides wide dynamic range for the modulation index and high DC link utilization while maintaining low harmonic levels that satisfy industrial standards.
The document summarizes the HortonMachine, a spatial analysis package integrated within the JGrass GIS system. It began as standalone routines in C and has been rewritten in Java and integrated into JGrass. The HortonMachine contains tools for DEM manipulation, geomorphology, network analysis, hillslope analysis, basin attributes, statistics, and hydrogeomorphology modeling. It implements hydrological analyses and aims to provide tools adhering to standards of the scientific community.
This document summarizes the key steps in cell planning and optimization for a GSM network in Sragen, Indonesia, including:
1) Conducting traffic and coverage analysis, dimensioning the nominal cell plan, and determining link budgets and site requirements.
2) Performing a detailed frequency plan, parameter planning, and interference predictions.
3) Installing and commissioning new sites, then conducting drive tests and optimizations to meet key performance indicators.
4) Ongoing radio frequency optimization is needed using statistics to identify and address problems impacting call setup success rate, handover success rate, or dropped call rate.
The document discusses various LTE measurement parameters and procedures including:
1. The eNB reports a list of detected PRACH preambles and measures timing advance, average RSSI, average SINR, UL CSI, and transport BLER for RRM purposes.
2. UE measurements include CQI, RSRP, and RSRQ while eNB measurements include timing advance, RSSI, SINR, UL CSI, detected preambles, and transport BLER. Inter-RAT measurements are also discussed.
3. Examples of RSRP, RSRQ, and timing advance procedures are provided along with CQI measurement details. PLMN selection, cell selection,
Radio measurements in long term evolutionVamsy Satish
This document discusses various LTE measurements including:
1. Preamble detection, transport BLER, timing advance, RSSI, SINR, CSI which are measured by the eNB.
2. UE measurements like CQI, RSRP, RSRQ and eNB measurements like transmit power and interference power.
3. Inter-RAT measurements from LTE to other systems like UTRA, GSM, CDMA2000 for handover purposes.
It provides examples and explanations of key measurements like RSRP, RSRQ, and timing advance. It also covers cell selection, PLMN selection and reselection procedures in idle mode.
Nasa tech briefs ksk 11495, simplified model of duct flowJulio Banks
This document provides technical details on a simplified model for analyzing transient duct flow, including:
- A one-dimensional model is developed using a perturbation of duct exit area to account for friction loss and relate transient to quasi-steady duct velocity with a differential equation.
- Computer programs are included that calculate duct exit momentum through an iterative momentum balance between inlet and outlet, incorporating engine shock loss and additional duct combustion.
- Validation shows the model correlates well with single engine helium and steam test data over a range of chamber pressures.
- Application to full-scale conditions indicates maximum air flow is less than actual Space Shuttle levels, suggesting helium flow alone cannot replicate critical conditions.
P&w tables of compressible flow functionsJulio Banks
Compressible-flow Mach Functionas
Page 5 - Nomenclature
Pages 6 & 7 - Mach Functions
Recommendaitons: Used Equations on Pp. 6 & 7 to
generate any of the results from the table as functions
of specific heat ration, Gamma = Cp/Cv.
Enjoy it as one would enjoy their favorite music.
The document describes default test templates in the Raptor HH device for testing various electrical equipment. It includes:
1. Templates for circuit breaker testing, overcurrent relay testing, current transformer testing, Rogowski coil testing, AC resistance measurement, ground grid testing, and CT burden testing.
2. Templates for voltage transformer testing, VT burden testing, and short-circuited potential transformer testing.
3. A template for measuring potential transformer ratios.
The templates allow automatic or semi-automatic testing of this equipment by selecting the appropriate template and configuring test parameters.
Study and Development of an Energy Saving Mechanical SystemIDES Editor
A new energy-saving mechanical system with
automatically controlled air valves has been proposed by
investigator and the preliminary model setup has been tested.
The testing results indicated the proper function of this
energy-saving mechanical system. This mechanical system
model has been simulated and analyzed by the computational
aided engineering solution. The major advantages of this
mechanical system include: simple and compact in design,
higher efficiency in mechanical functioning, quiet in
manufacturing operation, less energy losses due to less
frictional forces in this free piston-cylinder setup, selfadjustable
in operational parameter to improve the system
performance, and etc.
The document describes a series of use cases (UC-832, UC-833) for calibrating and running hydrological models in a common service. It involves downloading data, creating local models, calibrating models, performing simulations, and exploring results. Key steps include selecting areas of interest, adding observation stations, calibrating models using station data, running simulations with climate scenarios, and viewing output time series.
This document provides instructions for an experiment involving the regulation of a three-phase salient pole alternator. It includes the objectives, list of experiments, theory, circuit diagram, nameplate details, observations, calculations, precautions and procedures for conducting the slip test experiment to determine the alternator's regulation by varying the load and measuring voltages and currents. The goal is to calculate the direct axis and quadrature axis reactances and plot the regulation curves at varying power factors to understand the alternator's performance characteristics.
The document provides instructions for experiments to be conducted in the Control Systems Lab course at BTL Institute of Technology and Management in Bangalore, India. It lists 11 experiments involving designing and analyzing compensating networks, studying controller performance, and using MATLAB/SCILAB for simulations. The experiments are divided into two cycles, with the first cycle focusing on hardware implementations and the second on software simulations. Specific procedures are given for designing and characterizing lead and lag compensators.
ENHANCED DATA DRIVEN MODE-FREE ADAPTIVE YAW CONTROL OF UAV HELICOPTERijics
An enhanced data driven model-free adaptive yaw control tracking control scheme is proposed for the yaw
channel of an unmanned-aerial-vehicle (UAV) helicopter which is non-affine in the control input in this paper. Through dynamic linearization and observer techniques, the proposed control algorithm is only based on the pseudo-partial derivative (PPD) parameter estimation derived online from the I/O data of the yaw channel of an UAV helicopter, and Lyapunov-based stability analysis is utilized to prove all signals of
close-loop control system are bounded. Compared with the traditional model free adaptive control
(MFAC), the proposed enhanced MFAC algorithm can make the close-loop control system with stronger robustness and better anti-jamming ability. Finally, simulation results of the UAV yaw channel are offered to demonstrate the effectiveness of the proposed novel control technique.
A Simplified Speed Control Of Induction Motor based on a Low Cost FPGA IJECEIAES
This paper investigates the development of a simplified speed control of induction motor based on indirect field oriented control (FOC). An original PI-P controller is designed to obtain good performances for speed tracking. Controller coefficients are carried out with analytic approach. The algorithm is implemented using a low cost Field Programmable Gate Array (FPGA). The implementation is followed by an efficient design methodology that offers considerable design advantages. The main advantage is the design of reusable and reconfigurable hardware modules for the control of electrical systems. Experimental results carried on a prototyping platform are given to illustrate the efficiency and the benefits of the proposed approach.
Turbofan Engine Modelling and Control Design using Linear Quadratic Regulator...theijes
There are many applications in which gas turbine engine is used today, including aircraft propulsion for both commercial and military purposes, and power generation and in all these Control systems technology has played a fundamental role in enhancing performance. Modelling plays a significant role in the development of the entire engine system performance. This paper investigated Linear Quadratic Regulator (LQR) model-based control method to obtain estimates of performance parameters. The main control variable selected is the fuel flow to control the rotational speed of high-pressure spool speed of the turbofan engine. Firstly a suitable mathematical model of the engine is developed in MATLAB Simulink environment with both the intercomponent volume and the constant mass flow methods used. Equations of the mass flow rate and the torque balance are incorporated in the steady state and dynamic state of the thermodynamic engine model. This represents the engine model by a set of first-order differential and algebraic equations and a linearized model is extracted for the analysis and design of a controller by LQR. It is demonstrated that LQR based controllers can perform better than conventional PID controllers. The settling time, rise time and maximum overshoot for LQR based controller are all less than those for PID based controller. The input also changes more accurately for LQR than the PID controller compared.
Mobile instrumentation and_data_processing_system_for_testinglkantwani
This document describes a mobile instrumentation and data processing system for testing agricultural field machinery. The system collects data from sensors mounted on tractors and implements during field tests, including three-point hitch forces, PTO torque and speed, forward speed, wheel slip, fuel flow, and depth of work. Data is transmitted via radio telemetry to a vehicle where it is recorded and processed. The system provides processed data in the field to modify tests and identify performance issues. Field tests examined the effects of different soil contact pressures on soil and crops. The system allows efficient testing at remote field sites with real-time data analysis.
This document provides an overview of global positioning systems and flight management systems used in aircraft. It defines key terms and describes the components and functions of GPS, WAAS, INS, barometric altimeters, and how they integrate with an aircraft's flight management system. It explains how GPS and WAAS provide lateral and vertical navigation guidance for different types of instrument approaches, including LNAV, LNAV+V, LNAV/VNAV, LP, and LPV approaches. It also covers requirements, limitations, and safety aspects of using GPS and WAAS for navigation.
Automated Testing of C-Band Rotary Field Ferrite Phase ShifterIJERA Editor
This paper presents the methodology for an automatic test procedure based on LabVIEW for RF characterisation of C- band rotary field phase shifter. Using this software, the characteristics of the phase shifter intended for phased array application viz. differential phase shift, insertion loss, return loss, rms phase error, insertion phase are measured systematically and displayed graphically in user friendly format.
This document presents SEA, an experimental testing environment for electrohydraulic actuators. SEA allows for precise measurement of important actuator variables to enable comprehensive static and dynamic characterization. It includes a hydraulic pump and pipelines, configurable loads, an instrumented manifold for measurements, and a DAQ system. Experimental results from characterizing an aerospace actuator using SEA are provided, including static calibration, transient response testing showing high pressure and flow demands, and system identification to develop an input-output mathematical model. SEA provides an effective environment for full experimental characterization of electrohydraulic actuators.
The document proposes a switching strategy for space vector modulated current link inverters connected to the power grid. It discusses pulse width modulation techniques and space vector pulse width modulation. The proposed strategy uses symmetrical cell time switching sequences to realize the six current vectors and minimize harmonics. Analytical calculations and experimental results show the strategy provides wide dynamic range for the modulation index and high DC link utilization while maintaining low harmonic levels that satisfy industrial standards.
The document summarizes the HortonMachine, a spatial analysis package integrated within the JGrass GIS system. It began as standalone routines in C and has been rewritten in Java and integrated into JGrass. The HortonMachine contains tools for DEM manipulation, geomorphology, network analysis, hillslope analysis, basin attributes, statistics, and hydrogeomorphology modeling. It implements hydrological analyses and aims to provide tools adhering to standards of the scientific community.
This document summarizes the key steps in cell planning and optimization for a GSM network in Sragen, Indonesia, including:
1) Conducting traffic and coverage analysis, dimensioning the nominal cell plan, and determining link budgets and site requirements.
2) Performing a detailed frequency plan, parameter planning, and interference predictions.
3) Installing and commissioning new sites, then conducting drive tests and optimizations to meet key performance indicators.
4) Ongoing radio frequency optimization is needed using statistics to identify and address problems impacting call setup success rate, handover success rate, or dropped call rate.
The document discusses various LTE measurement parameters and procedures including:
1. The eNB reports a list of detected PRACH preambles and measures timing advance, average RSSI, average SINR, UL CSI, and transport BLER for RRM purposes.
2. UE measurements include CQI, RSRP, and RSRQ while eNB measurements include timing advance, RSSI, SINR, UL CSI, detected preambles, and transport BLER. Inter-RAT measurements are also discussed.
3. Examples of RSRP, RSRQ, and timing advance procedures are provided along with CQI measurement details. PLMN selection, cell selection,
Radio measurements in long term evolutionVamsy Satish
This document discusses various LTE measurements including:
1. Preamble detection, transport BLER, timing advance, RSSI, SINR, CSI which are measured by the eNB.
2. UE measurements like CQI, RSRP, RSRQ and eNB measurements like transmit power and interference power.
3. Inter-RAT measurements from LTE to other systems like UTRA, GSM, CDMA2000 for handover purposes.
It provides examples and explanations of key measurements like RSRP, RSRQ, and timing advance. It also covers cell selection, PLMN selection and reselection procedures in idle mode.
The document discusses various LTE measurement techniques including:
1. Preamble detection, transport BLER, timing advance, RSSI, SINR, CSI which are measurements performed by the eNB.
2. RSRP, RSRQ which are measurements performed by the UE to aid in cell selection and reselection.
3. Timing advance which involves the eNB estimating timing from the preamble and signaling a correction to the UE.
The document discusses various LTE measurement techniques including:
1. Preamble detection, transport BLER, timing advance, RSSI, SINR, CSI which are measurements performed by the eNB.
2. RSRP, RSRQ which are measurements performed by the UE to aid in cell selection and reselection.
3. Timing advance which involves the eNB measuring the timing of uplink transmissions from the UE and sending a timing advance command to adjust the UE's timing.
The document discusses various LTE radio measurements performed by the UE and eNB including:
1. The eNB measures timing advance, average RSSI, average SINR, UL CSI, and detected PRACH preambles to monitor UE signal quality and perform handovers.
2. The UE measures RSRP, RSRQ, CQI to determine signal quality and perform cell reselection and handovers.
3. Timing advance allows the eNB to measure the initial timing of UL channels and instruct the UE to adjust its timing to prevent interference.
The document describes a method for detecting and determining post-launch frequency shifts in channels on the AMSU-A instrument. The method uses satellite cross-over data and radiative transfer modeling to identify a frequency shift in Channel 6 on NOAA-15. The analysis finds the actual channel frequency is 36.25 MHz higher than the pre-launch measurement. This method could help improve weather forecasts by providing more accurate channel frequency data for assimilation of AMSU observations.
A low-power 2-bit/step operation technique is proposed which uses dynamic threshold configuring comparator instead of multiple digital-to-analog converters (DACs). Power and area overhead is minimized by successively activated comparators. The comparator threshold is configured by simple Vcm biased current source, which keep the ADC free from power supply variations over 10%. To implement power efficient and high performance analog-to-digital converters the designers are urged to design an optimized dual tail comparator. In this paper, It is shown that in the proposed dual tail comparator both the power and delay time is significantly reduced.
This document proposes an adaptive modulation scheme using rain fade predictions from Kalman filtering to mitigate the effects of rain fade on geostationary satellite communications in the Ka-band. It simulates a cognitive radio-based satellite communication system with an adaptive transmitter and receiver. Prediction of the rain fade using a linear Kalman filter allows time for the transmitter and receiver to reconfigure before the predicted fade occurs, improving the bit error rate performance by two orders of magnitude compared to a non-adaptive system. The simulation shows switching between 4-QAM and 16-QAM modulation based on predicted fade levels keeps the bit error rate below a threshold while transmitting more data overall.
This document provides a review of different position estimation methods for permanent magnet synchronous motors (PMSMs). It discusses indirect methods based on back electromotive force (EMF) detection, model-based methods using flux linkage or inductance estimation, and saliency-based methods using high frequency signal injection. Model-based observer approaches like extended Kalman filters are highlighted as effective for medium- and high-speed operation due to good disturbance rejection and robustness. The review evaluates the performance and limitations of different position estimation techniques for sensorless control of PMSMs.
This document discusses how Global Navigation Satellite Systems (GNSS) receivers and robotic total stations can be combined to provide an automated, accurate, and cost-effective system for monitoring large open-pit mines. Two main options for establishing a consistent reference frame are reviewed: using a network of total stations or combining total stations with GNSS receivers. The advantages of using GNSS receivers to provide absolute control from a stable location away from the mine are discussed. Practical considerations for implementing a combined total station/GNSS system are then presented, including installing the hardware and processing the data to ensure high accuracy.
This document outlines an 8-step process for calibrating a link-level 5G simulator based on an LTE link-level simulator. Each step validates a different component: 1) OFDM modulation, 2) channel coding, 3) SIMO configuration, 4) MIMO transmit diversity, 5) MIMO spatial multiplexing, 6) uplink, 7) alignment with 3GPP requirements, and 8) multi-link calibration. System-level calibration then occurs in two phases for LTE and LTE-Advanced technologies.
S-MAC is an energy-efficient MAC protocol for wireless sensor networks where nodes follow a listen-sleep cycle. Nodes synchronize their schedules by broadcasting SYNC messages. A node can be a synchronizer that independently chooses a schedule, or a follower that adopts the schedule of its neighbors. Adaptive listening is proposed to reduce latency by allowing nodes to wake up briefly after overhearing transmissions. Later protocols like DW-MAC and AS-MAC use scheduled wake-ups to improve energy efficiency while allowing variable length transmissions. Q-MAC and R-MAC incorporate routing by dynamically adjusting schedules for query and data transmissions between multiple hops to the destination.
LTE KPI Optimization - A to Z Abiola.pptxssuser574918
1. The document discusses LTE post launch optimization, including problem causes, solutions, and case studies.
2. It describes different types of counters used to collect PM statistics, including peg, gauge, accumulator, scan, PDF, DDM, calculated, trigACC, and trigSCAN counters.
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Similar to MC and WARR Callibration - Final Update (20)
2. MemberoftheHelmholtzAssociation
-Ground Wave is identified** in WARR trace, then cross-
correlated with the corresponding MC trace; the
“MC/WARR time-shift“ is then the time corresponding
to the maximum cross-correlation value 2
Context
-Previous Work:
a) Cross-Correlation Analysis of Baxter‘s July 2015 Selhausen MC/WARR Data*
(“t0-correction Update Pres” in FZJ-GPR)
-Overall Objective: To determine whether 500MHz multichannel GPR data can be calibrated
with CMP data acquired at corresponding locations, via modification of the t0-correction
-Based upon intuitive hypothesis that traces of the 2 surveys, at the same locations, are
similar but just time-shifted version of one another
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Context
Results:
-Same procedure is iterated over all other channels at the specific location, then
all channels at each and every other location
-A general, channel-specific t0-correction could not be established, due to evident
heterogeneity in the time-shift at different CMP locations along the 120m line
-Mix of time shifts both positive and negative; whereas a systematic shift
between MC/CMP data should be only one or the other?
-Necessitates focus upon only a few locations for subsequent measurements…
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b) Analysis of July 2016 Selhausen MC/WARR Data, including new MC-calibration
Measurements (Location=5m)
(“MC-Calibration Update” in FZJ-GPR)
-Channel 4 produces very low amplitudes, as well as energies (sum of squared amplitudes)
relative to other channels
-Script MC_calib_processing produces amplitude/energy plots, plots temporal cross-correlation
between measurements taken at different times, and wiggle (as opposed to colour traces)
-Can choose to exclude any combination of undesirable channels/positions from analysis
Context
Apply Channel-specific t0-correction
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*As determined by manual picking of 1st air-wave arrivals
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ContextResults:
-Calculated expected air-wave arrival times for every channel/location, based on
theoretical air wave velocity (0.2997m/ns)
-For any particular location on the MC-sled:
t0-Correction = Measured arrival time* - Theoretical arrival time
-Typically, channels 1/2/3/6 have similar t0-correction values, while channels 4/5/7
are also similar, albeit delayed relative to channels 1/2/3/6
-Chose to exclude Location 1 (at 23cm on MC-sled) for all channels, due to difficulties
in manual air-wave picking arising from near-field effects (see next slide)
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Calculation of Cross-Correlation
Coefficient for Quantitative Measure
of Deviation in Traces over Time-
Spans of a few seconds
(at 5m vs. 110m along profile)
-Position 1 removed from analysis
-Generally (except for Channel 4), value is >0.97,
indicating high degree of temporal self-similarity
(over scales of several seconds)
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Current Work: Data Comparison of
July 2016 Selhausen Measurements
Definitions
-Full WARR: Data that, aside from skipped traces, encompasses a continuous
range of offsets
-7 traces WARR (3 forms):
a) MC-sled I: Measurements taken with the MC-sled (termed “MC
-calibration measurements), during which a single-channel WARR is
performed for each and every channel (by varying the Rx-position
over all positions in the MC-sled, for each channel)
b) MC-sled II: Full WARR in MC-sled, that has later (via processing)
been reduced to the subset of 7 traces corresponding to MC positions
c) PE-sled: Same as (b), but with PE-sled
-PE-sled: Measurements taken with the Pulse Ekko single-channel sled
-MC-sled: Measurements taken with the custom multichannel sled
-Channel: A particular transmitter/receiver combination (eg. Tx/Rx4)
-Position/Location: The specific section into which Rx is placed
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Current Work: Data Comparison of
July 2016 Selhausen Measurements
Field Conditions/Measurements
-See spreadsheet Selhausen-04-07-MC in FZJ-GPR for detailed information regarding data files
-Field Measurements taken on 04/07/2016 with Manuela, Anja, Jan; survey design by Manuela
-Weather: Hot, sunny day with no rain
-DVL battery was running low for later measurements (ie. during CMP’s, 110m MC-calibration)
Data Processing Considerations
-Location of Interest: 5m along 120m profile (where 0m is the side closest to the street)
-Only performed all survey methods with Channel 1; Channels 2-6 were only used for MC-
calibration measurements at 5m and 110m, as well as for MOG of the entire 120m profile
-All traces dewowed (calls script dewow_anja_eso.m), ungained, and normalized to
max(abs(‘trace’))=1, to allow for comparison between MC/WARR data
-RPE_Evan.m indicates no skipped traces for MC-calibration data
-Output/Plots generated by script MC_calib_processing.m in main folder
-Semblance Analysis Parameter Space:
a) Ground Wave
- t0 ∈ (0,5) ns
- v ∈ (0.05,0.15*) m/ns
b) Air Wave (newly implemented)
- t0 ∈ (1.5,5.0) ns
- v ∈ (0.25,0.30) m/ns
a)/b) Parameters for both Air/Ground Waves
*Time width = 24ns (arbitrary..?)
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Script Documentation
GPR_Summer_2015_MC - Main script for MOG MC data along profile; must specify data
folder + line (only 1 permitted)
-Accounts for skipped traces by removing them, then compressing the data-set
-Only need to do air-wave picks once; upon completion, will save and use picks
in future
To redo picks, delete t0AirOffsets.mat
Velocity_Analysis_MC_Automated- Called by above - main script for automated ground-
wave picking from MC-data (semblance takes in as input each ‘7-trace WARR’ taken by
the MC system); includes t0-correction and no smoothing
MC_calib_processing – Script to process 7-trace WARR (MC-sled I) data
-Can choose whether to do manual air-wave picks or automated ones (ie. air-
wave semblance); ground-wave picking automated via semblance
-Can exclude any combination of channels/positions from analysis in section
‘Data Parameters’, sub-section ‘MC-calibration Parameters’
Velocity_Analysis_MC_Automated_calib – Similar to Velocity_Analysis_MC_Automated,
but for 7-trace WARR (MC-sled I) data
Velocity_Analysis_MC_Automated_calib_wiggle – Same as above, visualized as
wiggle-traces rather than colour plots
Velocity_Analysis_MC_Automated_calib_wiggle_airground – Same as above, with
automatic air-wave semblance picking instead of manual air-wave picking
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Script Documentation
GPR_Summer_2015_WARR – Main script for WARR data (of form MC_sled II or PE_sled)
-Smooths data (5-point moving average)
Saves air-wave picks; to redo, delete xairpicks or tairpicks (deleting either one
will re-write both)
vel_ana_TE_CO_CMP_Multi_Automated – Called by above; automatic pick of maximum
semblance to determine ground wave
vel_ana_TE_CO_CMP_Multi_Comp – Similar to above, but with manual pick of maximum
semblance (Igor has incorporated into his scripts)
CMPandMC_correlation – Main script used previously for cross-correlation analysis of
Baxter’s July 2015 Selhausen data
PlotAllSelectTraces – Plots the 3 types of 7-trace WARR surveys (see (a)/(b)/(c) in
‘Definitions’) at all offsets
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-t0-correction now
applied, based on
direct air-wave pick
(value displayed at
bottom of plots)
-Semblance analysis
used to (attempt to)
identify ground wave
(bolded line on plots)
T0-correction +
Corresponding
Semblance
(High-freq.
air picks)
PE-sled
MC-sled
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Analogous
plots for Low-
Freq. air picks
PE-sled
MC-sled
-Difference in t0-
correction when choosing
high vs. Low-freq. Air
wave is ~6ns for both
PE/MC-sleds
-PE-sled pick appears
~correct (characterizing
the ground wave
minimum)
-MC-sled pick in-correct;
ostensibly requires
inclusion of negative
intercept-time in
semblance parameter
space?
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11:05
15
Full WARR PE-sled, at Different Time, t0-corrected/gained
11:09 12:56
-Compare whether picking high vs. low frequency air-wave has effect upon
temporal variation of t0 (over the course of the day)
High-frequency Picks
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-For low-frequency picks, max
semblance (and associated
values of t0/v) are far more
consistent, than amongst high-
frequency picks
Implies that minimization of
temporal variability requires
picking of low-frequency air-
waves, even if earlier high-
frequency content is present
Corresponding
Semblance Plots
High-frequency
picks
Low-frequency
picks
11:05
11:05
11:09
11:09 12:56
12:56
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-t0-correction now relies upon (newly implemented) air-wave
semblance, replacing manual picking
General Proviso: Automatic air-wave picking requires fine-
tuning of parameter space!
-Chosen intercept time from air-wave semblance typically
too small (ie. Needs to be later to accurately plick 1st-
break)
-Optimal parameter space here is:
v ∈ (0.25* , 0.30) m/ns
t ∈ (0.18 , 5) ns
-No set of parameters tested thus far has resulted in 100%
accurate picking: typically there is a pattern in which though
most channels are fine, a few channels will have their automatic
pick being too early, for all locations at such channels (for
instance, the plots on Slide 20)
7-trace WARR (MC-sled): Gained vs. Ungained
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-Gaining of 7-trace WARR (MC-sled) data results in ambiguous
semblance plot (very high-values across parameter space, no
clear maximum), while ungained data contains several peaks
Observations
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Observations
-Effect of cable position appears significant, and may
affect accuracy of both air and ground wave picks
though it appears to influence the presence of early
-Channel 1: Plots for both positions identical upon
visual inspection
-Channels 2-6: 1st-break air wave arrival appears to be
delayed when cables on side, relative to those for the
cables on centre
-Can further investigate with cross-correlation, see if
cable position has influence on semblance results,
etc..
Require a ‘cable-holder’ that will allow for centre
position to be employed?
31. MemberoftheHelmholtzAssociation
Discussion: Sources of Uncertainty
a) Skipped Traces: Typically a few skips per CMP – if too many skips, can distort
linearity of air/ground wave, and therefore distort the t0 obtained from semblance
-Current method used in Ekko2Dread2_Update_test removes skipped
traces, then collapses data to remove the holes
-Offset information in header files has been corrected, to account for
skipped traces
-However, the data is not located in the correct position (offset), due to
collapsing approach
-Proposed Solution: Rather than collapsing data, fill in holes via
interpolation (eg. spline)
-See “On Recovering Missing Ground Penetrating Radar Traces by
Statistical Interpolation Methods” (Safont et. al. 2014) for inspiration?
b) Temporal Variation of t0 even for the same Survey Type*: Across multiple
measurements over the same day of the same thing (Full WARR at 5m in PE-
sled), is variable (see next slide)
-Possibilities: Instrumental temporal drift, use of high-frequency air
waves during manual picking
31
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Conclusions
Analysis of Channels in the Multichannel GPR System
-Channel 4 is faulty (very low amplitude/energy), rendering air-wave picking
(and consequently t0-correction) highly imprecise
-Channels 5/7 have sufficient energy, but on average have larger t0-values
than channels 1/2/3/6
-The channel-specific t0-correction may be dependent upon the specific
subsurface conditions at the location (eg. high-conductivity), as implied by the
fact that the 110m calibration measurements showed that even for different
positions of the same channel, t0 was variable; while calibration at 5m
produced much more consistent results
-Attempted CMP measurements with the Multiplexer failed
-Placement of the MC antenna cables on the middle vs. side of the sled
appears to have a significant effect for Channels 2-6, with the side positioning
resulting in a delayed air-wave 1st-break
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Conclusions
Semblance Analysis
-Semblance analysis breaks down (manifested by non-unique maxima,
non-physically reasonable parameters chosen,etc.) under circumstances
such as:
-Wave non-linearity (whether due to skips or otherwise)
-Use of only selected traces (eg. In MC)
-Gaining of data (for 7-trace WARR with the MC-sled)
-Generally, the Semblance Parameter space must be tested for each
data-set
-It is not always clear that 5ns is optimal as the maximum possible
intercept-time for 500MHz data; as max semblance values sometimes
occur at the edge of the parameter space
-Time-width (current default value of 24ns seems arbitrary)
Temporal Variation
-Temporal variation in data on the scale of several seconds is minimal,
as indicated by cross-correlation calculations; regarding diruanl
variations, the t0-correction value is also consistent, but only provided
that the low-frequency air-wave arrivals are chosen
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1. Apply the Channel-1 t0-calibration results to other channels; repeat
semblance, see if results are consistent across channels
2. Apply channel-specific t0-corrections (calculated from
MC_calib_processing.m) to the 120m profile MOG data, then see if
ground-wave semblance values become comparable with WARR data
taken at same positions
3. Perform 7-trace WARR (MC-sled) measurements at locations with a
range of conductivities, so as to better characterize the degree to which
the consistency of the channel-specific t0-correction is affected by
specific subsurface conditions at each location
Future Directions
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4. Implement potential Semblance Solutions, such as:
-Application of Hilbert Transform to 7-trace WARR (PE-sled)
may be an avenue for improvement of semblance and reduction of non-
uniqueness of maxima
-Investigation of the influence of Time-width (‘window’) on max
semblance picks
-Include negative time values in semblance parameter space?
5. Investigate proper treatment of skipped traces, via interpolation
6. Use filtering to improve air-wave picking, such as band-pass, to
remove high-frequency content sometimes seen, as well as low-
frequency waves that occur before the air wave
7. Construct/Upgrade MC-sled such that all antenna cables may be run
through the centre of the sled
Future Directions