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    List ofsuparco projectsforuniversities List ofsuparco projectsforuniversities Document Transcript

    • With the mission to promote industry-academia collaboration SUPARCO has taken this initiativeto involve university students to undertake meaningful projects which could contributesignificantly towards fulfilling SUPARCO’s objectives. As an incentive SUPARCO will recompensea minimum amount of Rs. 10,000/- for successful completion of each project. A list of projectsalong with level of assignment is tabulated hereunder: LIST OF SUPARCO PROJECTS FOR UNIVERSITIESS. NO. PROJECT TITLE LEVEL PAGE 1. Student Satellite Project Faculty 5 2. Design and Analysis of a 1 MW Wind Turbine Rotor Graduate 8 Software based onboard data handling simulator for 3. Graduate 9 functional verification CFD analysis of supersonic flow over slender cylindrical 4. Undergrad 10 bodies Damage characterization of composite materials under 5. Undergrad 11 impact loading 6. Design and development of Bit Synchronizer Undergrad 12 Design and development of pitch & yaw control of 7. Undergrad 13 air/water pressure nozzle in closed loop 8. S-Band Frequency Synthesizer Undergrad 14 9. Implementation of AES Encryptor/Decryptor on FPGA Undergrad 15 10. Remote transfer of large images Undergrad 16 11. Drought, Floods/ Environment related Studies Undergrad 17 12. Pitch Control of Movable Nozzle Model Undergrad 18 Page 1 of 58
    • 13. Smart-phone based GPS positioning Undergrad 19 Modeling and autonomous control of wheeled robot with14. Undergrad 20 obstacle avoidance Precise position and speed control of Dc servo motor for15. Undergrad 21 variable load16. SPI TO SPORT CONVERTER Undergrad 2217. Moving target detection and locking with moving camera Undergrad 23 Wireless Image and Video communication between DSP18. Undergrad 24 and PC Development of Android based application for home19. Undergrad 25 automation Design and Fabrication of RC PWM compatible drive for a20. Undergrad 26 four wheel differential drive robotic platform Design of integrated wireless Video/Audio21. Undergrad 27 transmitter/receiver of minimum 300 m range22. Learning techniques of Analog DSP (21065L) Undergrad 2823. DSP based high speed data Acquisition System Undergrad 29 Development of calibration scheme for Strapdown24. Undergrad 30 Inertial Navigation system A portable system for acquiring Analog and Digital data25. Undergrad 31 during field testing Design of a Universal DC motor torque vs Speed26. Undergrad 32 Measurement Scheme27. Flight Simulator Software Undergrad 3328. Inertial Navigation System for low speed vehicles Undergrad 3429. Remote sensing of physical parameters Undergrad 35 Page 2 of 58
    • 30. Stabilized Platform Controller Undergrad 36 Implementation of JPEG2000 Image Compression31. Undergrad 37 Software Using KAKADU_V2.2.3 Design and development of CPLD board for generation of32. Undergrad 38 timing signals for CCD sensors Design and development of speed and position controlled33. Undergrad 39 platform for Linear Image Sensor34. Design and development of high speed ADC module Undergrad 4035. Design of a Schmidt Cassegrain telescope Undergrad 4136. Design of a Ritchey Chretien telescope Undergrad 42 Power Management and Control System Microcontroller/37. Undergrad 43 FPGA based Variable Switching Power supply of 5-30volt output @38. Undergrad 44 6ampere DSP/FPGA implementation of Kalman filter based sensor39. fusion algorithm for attitude sensors (gyroscope, Undergrad 45 accelerometer/sun-sensor and magnetometer) DSP/FPGA implementation of high fidelity orbit40. Undergrad 46 propagator Analysis of space and time (memory and processing)41. complexities of different pattern matching algorithms for Undergrad 47 star identification PCB Analysis of Vertex-V FPGA Board using HYPERLYNX42. Undergrad 48 7.7 JTAG TAP Controller for Satellite On-board Configuration43. Monitoring and Control for Reliable System Undergrad 49 Implementation CCSDS based Packet Data extraction software of Remote44. Undergrad 50 Sensing Satellite Image Data Design and Development of CCSDS based Concatenated45. Reed Solomon Decoder & Viterbi Decoder along with de- Undergrad 51 Interleaver Software Page 3 of 58
    • Study of Reliable System Design Techniques like ( Triple46. Modular Redundancy (TMR)) for increasing the reliability Undergrad 52 of Embedded System in Space Design of Triple Modular Redundancy (TMR) based scheme for PowerPC based Payload System incorporating47. Undergrad 53 DDR2 memory and FPGA based Endpoint Devices for LEO satellite Study of EDAC(Error Detection and correction) Scheme48. Undergrad 54 for DDR memory for space application Analysis of space and time (memory and processing)49. complexities of different pattern matching algorithms for Undergrad 55 star identification50. Wind Resistant Stability of Tubular Wind Turbine Towers Undergrad 56 Manufacturing and Assembling of Tubular Towers of51. Undergrad 57 Wind Turbine To Study Flow Characteristics around Straight and Curved52. Undergrad 58 Fin Projectiles Page 4 of 58
    • STUDENT SATELLITE PROJECTOverview of Satellite Design 1. IntroductionDesign and development of satellite is a challenging tasks, at one hand it involves the teameffort of multiple disciplines and on the other designers need to ensure that satellite will beable to withstand and survive the harsh environment including temperature extremes,radiations, shocks, vibration during launch etc. Till today thousands of satellites have beenlaunched for various applications such as Weather Forecasting, Television Broadcasting,Communications, Internet Communications, Navigation, and Remote Sensing etc. For any kindof satellite three components are required  Launcher (means to send it to desired orbit)  Satellite itself  Ground Station (means to control satellite and receive its data)The brochure at hand gives an overview of satellite design and various aspects that need to beconsidered. Simplified block diagram of a satellite is given below: Figure: Simplified Satellite Block diagram Page 5 of 58
    • SUBSYSTEM KEY TASKS TECHNOLOGIESStructure & Provides mechanical support to all subsystems and provide means to change Aerospace, Mechanical,Mechanism the configuration such as deployment of antennas etc Mechatronics,Power Generates, Stores, Regulates & Distributes Electrical power to all equipments Electrical, Electronics,Subsystem on board. Solar cells along with batteries are commonly used. Mechatronics,Communication Receives command from ground, demodulates them and send to data Electronics, RF,Subsytem handling unit. Similarly it transmits payload and engineering data to ground Microwaves station.C&DH Command & Data handling monitors on-board equipment operations and is Electronics, ComputerSubsystem responsible for handling data. SciencesAOCS AOCS keeps satellite in correct orientation. It consists of sensors (Horizon Aerospace, Mechanical,Subsystem Sensor, Sun Sensor, Star Sensor, GPS etc ), actuators (Gravity Gradient Mechatronics, Boom, Magneto Torquers, Momentum Wheel, Reaction Wheel, etc) and Electrical, Electronics, processor with controlling algorithms for correction. Computer ScienceThermal Maintains temperature of all equipment within allowable limits. It may use Aerospace, Mechanical,Subsystem coatings, insulation blankets, heat pipes or by using active techniques such as Space Sciences heaters, louvers etcPayload Payloads may be for Remote Sensing, Experimental instruments, Electrical, Electronics, Communications. Generally they involve image acquisition, digitizing, RF, Microwaves, compression, encoding, processing, modulation, amplification, filteration and Optics, Space Sciences communication.Ground Station Communicates with Satellite, receives health data and sends command. Electronics, RF, Microwaves, Power Subsystem Communications Subsystem Communication Links Page 6 of 58
    • C&DH Subsystem Ground Subsystem1. LIST OF EXEMPLARY EXPERIMENTS/ 1. SUPARCO AVAILABLE FACILITIES FOR SATELLITE PROJECTS DESIGN & DEVELOPMENTa. Satellite tracking experiment a. Thermal Vacuum Chamberb. Digital radio communications i. Simulate space environment (Vacuum). o oc. Digital Store & Forward communications ii. Temperature range from – 70 C to 100 C.d. Technology demonstration b. Satellite Assembly, Integration & Testing Facilitiese. Signal Intelligence i. Clean room required for integrating sensitive equipment.f. Remote Sensing ii. Testing of complete satellite (system level testing).g. Etc. iii. Can accommodate satellites of various sizes. c. Satellite Research & Development Centers2. SUPARCO INVOLVEMENT i. Development of various hardware and software for satellitea. Program Management subsystems. i. Student Project Manager and Chief Engineer ii. Development of various testing platform for satellite. ii. Student Subsystem Teams d. Anechoic Chamberiii. Engineering support for some critical tasks. i. Antenna Testing Facility.iv. Providing critical feed-back e. Helmholtz Coil Facility i. Magnetic devices testing and calibration.b. Faculty and Staff Engineering Mentorship (Know ii. Simulation of desired magnetic filed in all axes. How Transfer) i. Faculty Principal Investigator ii. Engineering Project Manager from Spaceiii. Mentor Engineers for Subsystems (e.g. instruments, structures, etc.)iv. Faculty Technology Advisorc. Engineering Mentorship, design reviews i. Environmental Testing Page 7 of 58
    • PROJECT TITLE Design and Analysis of a 1 MW Wind Turbine RotorOBJECTIVES Development of rotor for Horizontal Axis Wind TurbinePROJECT OUTLINE  Literature Review  To generate blade and hub profile  Grid independence study  Validation of CFD results  Investigation of flow around blades  Calculation of loads on blade and comparison with BEM method  Blade and hub profile optimizationMAJOR EQUIPMENT & Standard CFD SoftwareSOFTWAREREQUIREDDELIVERABLES  Methodology for the design of blade and hub profile  Solid model, grid, and solution files of design profile  ReportESTIMATED One YearDURATIONSPONSORING WING Space Technology (ST) Page 8 of 58
    • PROJECT TITLE Software based onboard data handling simulator for functional verificationOBJECTIVES To develop a software based simulator system for onboard data handling of a small remote sensing spacecraft (including pass simulation)PROJECT OUTLINE This simulator will use any standard remoting technique (like .NET remoting or AS3 remoting) to access remote object (simulating connectors) working on other systems connected using LAN. This simulator should comply 4th Step of Simulation Steps i.e. “Software in Loop”MAJOR EQUIPMENT & Matlab/ C++SOFTWAREREQUIREDDELIVERABLES A GUI based software in which if one value changes(push button for instance) on output pin of a connector the value is updated on the input (LED for instance) of corresponding connectorESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 9 of 58
    • PROJECT TITLE CFD analysis of supersonic flow over slender cylindrical bodiesOBJECTIVES Aerodynamic characterization of slender nose-cone-cylindrical projectilesPROJECT OUTLINE  Literature Review  CFD analysis of slender nose-cone-cylindrical projectiles  Grid independence study  Validation of CFD results with available experimental dataMAJOR EQUIPMENT & Standard CFD SoftwareSOFTWAREREQUIREDDELIVERABLES  Solid model, grid, and solution files of all configurations  ReportESTIMATED One YearDURATIONSPONSORING WING Space Technology (ST) Page 10 of 58
    • PROJECT TITLE Damage characterization of composite materials under impact loadingOBJECTIVES To study the impact resistance of composite materialPROJECT OUTLINE  Literature review  Finite Element Analysis of impact loading using ANSYS LSDYNA (Details of projectile will be provided)  Validation of FEA results through experimental testing (optional)  Report writing & presentation  Functionality will be damage characterization of wind turbine blade, composite helmets, composite CNG cylinder etcMAJOR EQUIPMENT &  FEA ToolSOFTWARE  Different composite couponsREQUIRED  Impact testing rig for experimental testing (optional)DELIVERABLES  Characterization of damage area w.r.t. projectile size & velocity  Area of plastic damage on composite materials based on their type  Stress field due to damage & its role in subsequent life of structureESTIMATED One YearDURATIONSPONSORING WING Space Technology (ST) Page 11 of 58
    • PROJECT TITLE Design and development of Bit SynchronizerOBJECTIVES To design and develop a bit synchronizer which can input Manchester encoded serial data and output data in NRZ-L form with a synchronized clockPROJECT OUTLINE • Input data bit rate: 32K,64K,128K,192K,256K,512K,1M(selectable) • Input data level: 0-2 Vp-p • Input data code: Manchester encoded data • Output data format: NRZ-L • Output data level: 0-5 V (TTL) • Output clock level: 0-5 V (TTL) • Output clock phase: 0° and 90° (Selectable)MAJOR EQUIPMENT & Logic state analyzerSOFTWAREREQUIREDDELIVERABLES A plug and play hardware system to fulfill the requirements mentioned in specification tableESTIMATED One YearDURATIONSPONSORING WING R&IW Page 12 of 58
    • PROJECT TITLE Design and development of pitch & yaw control of air/water pressure nozzle in closed loopOBJECTIVES To gain command over mechanical design and control of Electro Mechanical systemPROJECT OUTLINE • +/- 45 degrees angle of freedom in pitch and yaw, pot/encoder mounted on each pitch yaw axes for feed back • Nozzle sizes can be chosen to ease manufacture and procurement • Linkage sizes etc can be varied to fulfill conceptual and functional requirements • Simultaneous pitch/yaw operation (desired but not necessary)MAJOR EQUIPMENT & Matlab/ Simulink/ Controls ToolboxSOFTWAREREQUIREDDELIVERABLES Functional model of pitch yaw control in closed loopESTIMATED One YearDURATIONSPONSORING WING R&IW Page 13 of 58
    • PROJECT TITLE S-Band Frequency SynthesizerOBJECTIVES Design and development of S-Band Frequency SynthesizerPROJECT OUTLINE • Study of Basic Microwaves, Control Theory. • Study of Phase Locked Loop theory. • Study of different types of filters especially active filters. • Design and simulation • Development of hardwareMAJOR EQUIPMENT & Network analyzerSOFTWAREREQUIREDDELIVERABLES Production of Local Oscillator on hardware with SMA connector at the o/p port , Comprehensive ReportESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 14 of 58
    • PROJECT TITLE Implementation of AES Encryptor / Decryptor on FPGAOBJECTIVES Development of AES Encryptor/ Decryptor on FPGAPROJECT OUTLINE • Study of Information Security and Cryptography • Study of FIPS PUB 197 standard • Selection of AES parameters • HDL Coding & Testing on FPGA Platform • Analysis of memory management, decoding delayMAJOR EQUIPMENT & Standard FPGA KitSOFTWAREREQUIREDDELIVERABLES Timing Simulation, FPGA implementation and ReportESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 15 of 58
    • PROJECT TITLE Remote transfer of large imagesOBJECTIVES Secured and efficient transfer of large size imagery to a hand held devicesPROJECT OUTLINE • Study of large imagery handling in a limited memory environment • Remote streaming of large size imagery • Develop a data security mechanism over the air • Efficient handling of imagery using handheld devices • Develop multi tier application for remote accessMAJOR EQUIPMENT & Appropriate standard softwareSOFTWAREREQUIREDDELIVERABLES Multi tier application along with algorithm, Comprehensive ReportESTIMATED One YearDURATIONSPONSORING WING Space Application Research Page 16 of 58
    • PROJECT TITLE Drought, Floods/ Environment related StudiesOBJECTIVES Environmental Protection and Damage Assessment / AdaptationPROJECT OUTLINE • Basic Studies about the Environment • Study of impact of Hazards Like Floods on Environment • Use of Satellite Remote Sensing(SRS) in Environmental Monitoring • Report on the existing conditions/ RecommendationsMAJOR EQUIPMENT & Appropriate related imageriesSOFTWAREREQUIREDDELIVERABLES Comprehensive report on the current state of the environmentESTIMATED One YearDURATIONSPONSORING WING SPAS/SAR Wing Page 17 of 58
    • PROJECT TITLE Pitch Control of Movable Nozzle ModelOBJECTIVES To learn the Design and Development of Thrust Control Nozzle ModelPROJECT OUTLINE A picture speaks thousand words. The picture above describes the project outlineMAJOR Nozzle, Electromechanical Actuator, Torsion Spring, Gas Cylinder,EQUIPMENT & Piping, Fitting Components, Controller,SOFTWAREREQUIRED PRO/E , AutoCADDELIVERABLES Mechanical Hardware and Design ReportESTIMATED One YearDURATIONSPONSORING WING R&IW Page 18 of 58
    • PROJECT TITLE Smart-phone based GPS positioningOBJECTIVES The aim of the project is to develop android based application which can transmit real-time position information from smart phone to personal computer (PC)PROJECT OUTLINE In this project, android based application will be develop which will extract real-time position from the GPS-chip embedded in the smart- phone and transmit this extracted position to the PC for real time visualizationMAJOR EQUIPMENT &  Smart-phoneSOFTWARE  Android application development suiteREQUIRED  Internet connectivityDELIVERABLES Android based smart-phone capable of transmitting real-time position information to the PCESTIMATED One YearDURATIONSPONSORING WING R&IW Page 19 of 58
    • PROJECT TITLE Modeling and autonomous control of wheeled robot with obstacle avoidanceOBJECTIVES  Development of control algorithm  Development of optimal path selection algorithm to cater with obstaclesPROJECT OUTLINE In this project, the teams members will develop an autonomous 4 wheeled robot which accurately reaches target coordinates and follows the given profile by taking the starting point as initial position (0,0). In the presence of an obstacle, a search algorithm will be devised to avoid obstacles and efficiently attain the target pointMAJOR EQUIPMENT &  4 wheeled vehicleSOFTWARE  Digital signal processorREQUIRED  C-languageDELIVERABLES  Demonstration of four wheeled robot to follow the required profile in presence of obstacles  Project report  SoftwareESTIMATED One YearDURATIONSPONSORING WING R&IW Page 20 of 58
    • PROJECT TITLE Precise position and speed control of Dc servo motor for variable loadOBJECTIVES  Development of control algorithm for speed and position control  The designed system is capable to achieve desired position and rate with various loading conditionsPROJECT OUTLINE In this project the team members will develop the precise control algorithm for DC motors under the presence of load (platform) to accurately achieved the required position or rotating with various rates given by the user, through an interfaceMAJOR EQUIPMENT &  DC Servo MotorsSOFTWARE  DC drivesREQUIRED  Development of an interface to command desired position or rate  C-LanguageDELIVERABLES  Demonstration of precise position and speed control of DC motors  Project report  Electronic circuit design and softwareESTIMATED One YearDURATIONSPONSORING WING R&IW Page 21 of 58
    • PROJECT TITLE SPI TO SPORT CONVERTEROBJECTIVES Develop a module that can facilitate interface between SPI device and SPORT devicePROJECT OUTLINE Since there is no standard protocol or device that can facilitate interface between two devices working on SPI protocol and SPORT protocol respectively. So the main purpose of this project is to build a module based on microcontroller or some integrated circuits that allows the two devices working on different protocol to communicate with each other in an efficient mannerMAJOR EQUIPMENT &  SPI DeviceSOFTWARE  MicrocontrollerREQUIRED  SPORT DeviceDELIVERABLES  Properly Working Converter module  ReportESTIMATED One YearDURATIONSPONSORING WING R&IW Page 22 of 58
    • PROJECT TITLE Moving target detection and locking with moving cameraOBJECTIVES  Development of image and video data acquisition and processing software  The system is capable to lock moving object with still as well as moving cameraPROJECT OUTLINE In this project the team members will develop the image and video acquisition and processing algorithm implemented on DSP to identify and lock the moving object with still as well as with moving cameraMAJOR EQUIPMENT &  DSP boardSOFTWARE  CameraREQUIRED  Data acquisition interfaceDELIVERABLES  Demonstration of detection of moving object  Project report  Image acquisition and processing algorithmESTIMATED One YearDURATIONSPONSORING WING R&IW Page 23 of 58
    • PROJECT TITLE Wireless Image and Video communication between DSP and PCOBJECTIVES Development of wireless communication link between DSP and PC. The system is capable to transfer data for range of 200mPROJECT OUTLINE In this project the team members will develop wireless communication channel to transfer image and video stream to PC from a DSP over the range of around 200m. A GUI will be developed for the display of image and video on PCMAJOR EQUIPMENT &  DSP boardSOFTWARE  CameraREQUIRED  Wireless transmitter & receiver  Desktop PCDELIVERABLES  Demonstration of Video and image transmission over wireless link  Project report  SoftwareESTIMATED One YearDURATIONSPONSORING WING R&IW Page 24 of 58
    • PROJECT TITLE Development of Android based application for home automationOBJECTIVES Development of Android based application for home automation system for security and surveillance. The system is capable to cover a range of 100mPROJECT OUTLINE In this project the team members will develop Android based application for performing several applications from mobile set. The applications includes image acquisition from camera, capable to ON and OFF certain switches etcMAJOR EQUIPMENT &  Mobile setSOFTWARE  CameraREQUIRED  Wireless transmitter and receiverDELIVERABLES  Demonstration of designed application either using blue tooth or through internet to perform several applications for home automation  Project report  SoftwareESTIMATED One YearDURATIONSPONSORING WING R&IW Page 25 of 58
    • PROJECT TITLE Design and Fabrication of RC PWM compatible drive for a four wheel differential drive robotic platformOBJECTIVES Design and software/breadboard testing of a RC PWM drive capable of driving a four wheel differential drive vehicle Fabrication and testing of RC PWM drive capable of driving a four wheel differential drive vehiclePROJECT OUTLINE  Design of drive electronic and thermal design  Capability to operate the differential drive vehicles via commercially available RC transmitter receiver  Capable of driving PMDC up to 60 Volts and 30 Amp per motor  Thermal design  Drive hardware box  Testing on real systemMAJOR EQUIPMENT & Oscilloscope, Multimeter, Function Generator, Power supply,SOFTWARE Soldering Station, Bread board Proteus etcREQUIREDDELIVERABLES  Report on the design  Electronic hardware/boxESTIMATED One YearDURATIONSPONSORING WING R&IW Page 26 of 58
    • PROJECT TITLE Design of integrated wireless Video/Audio transmitter/receiver of minimum 300 m rangeOBJECTIVES Design and simulation of wireless Video/Audio transmitter/receiver which can work in 300 m line-of-sight rangePROJECT OUTLINE  Transmitter capability of accepting A/V input from camera/microphone  Receiver output in PAL/NTSC (colour)  Working range required to be 300 m line-of-sight  Testing of designed system on software and available hardwareMAJOR EQUIPMENT & Oscilloscope, Multi meter, Function Generator, Power supply,SOFTWARE Soldering Station, Bread board Proteus etcREQUIREDDELIVERABLES Design reportESTIMATED One YearDURATIONSPONSORING WING R&IW Page 27 of 58
    • PROJECT TITLE Learning techniques of Analog DSP (21065L)OBJECTIVES To learn techniques for programming of Digital Signal Processor(21065L)PROJECT OUTLINE Introduction to VDSP++ and ADSP (21065L)  How to create a new project  What are bios functions  Comparison to C language (loops/conditions/data types etc)  Memory architecture  SPORT architecture  IO flags architecture  UART architecture  etc. Practical Programming of DSPMAJOR EQUIPMENT & DSP Development Board ADSP-21065L, Visual DSP++ 5.0, A PC withSOFTWARE serial port. , Power Supply and Required CablesREQUIREDDELIVERABLES ReportESTIMATED One YearDURATIONSPONSORING WING R&IW Page 28 of 58
    • PROJECT TITLE DSP based high speed data Acquisition SystemOBJECTIVES Design and development of a data acquisition system by using DSP (21065L) and 16 bit ADC (AD73360)PROJECT OUTLINE • Study of DSP and ADC • Hardware Design • Hardware and software Development • TestingMAJOR EQUIPMENT & Matlab, LabviewSOFTWAREREQUIREDDELIVERABLES DAQ System circuit and softwareESTIMATED One YearDURATIONSPONSORING WING R&IW Page 29 of 58
    • PROJECT TITLE Development of calibration scheme for Strapdown Inertial Navigation systemOBJECTIVES Development of calibration scheme for INS having DTG’s and Pendulous accelerometers in orthogonal configuration with reference surfacesPROJECT OUTLINE • Error Model of Inertial sensors • Rate Calibration • Position Calibration • Computation • Software DevelopmentMAJOR EQUIPMENT & Matlab, LabviewSOFTWAREREQUIREDDELIVERABLES Calibration Scheme SoftwareESTIMATED One YearDURATIONSPONSORING WING R&IW Page 30 of 58
    • PROJECT TITLE A portable system for acquiring Analog and Digital data during field testingOBJECTIVES A portable system for acquiring Analog and Digital data during field testingPROJECT OUTLINE • Programming of u-controller • Software development for PC interfacing • Development of hardware for data acquisition • Data Processing & representation • Field TestingMAJOR EQUIPMENT & Matlab, Labview, CSOFTWAREREQUIREDDELIVERABLES Hardware + SoftwareESTIMATED One YearDURATIONSPONSORING WING R&IW Page 31 of 58
    • PROJECT TITLE Design of a Universal DC motor torque vs Speed Measurement SchemeOBJECTIVES Familiarization of different motors and to gain command over mechanical design and control of Electro Mechanical systemPROJECT OUTLINE  Project involves design of DC motor torque and speed measurement rig  Design will be based on testing of low profile DC motors  Motors will be tested around an angle of ± 40 Degrees  Torque and speed sensors should be utilized for measurement feedback  Torque testing range is around ±150 Nm  Completion time will depend on number of students working and time available to them (tentative is about 4-6 months)MAJOR EQUIPMENT & MatlabSOFTWAREREQUIREDDELIVERABLES Functional modelESTIMATED One YearDURATIONSPONSORING WING R&IW Page 32 of 58
    • PROJECT TITLE Flight Simulator SoftwareOBJECTIVES Software development of 6 DOF flight simulatorPROJECT OUTLINE  Study of 6 Degree of freedom motion  Study of Flight simulator  Study of different programming environment  Software developmentMAJOR EQUIPMENT & Matlab, LabviewSOFTWAREREQUIREDDELIVERABLES Design report and softwareESTIMATED One YearDURATIONSPONSORING WING R&IW Page 33 of 58
    • PROJECT TITLE Inertial Navigation System for low speed vehiclesOBJECTIVES Develop an inertial navigation system algorithm in embedded system using inertial sensor dataPROJECT OUTLINE  Study of inertial sensors  Study of navigation principles  Study of embedded systemsMAJOR EQUIPMENT & MatlabSOFTWAREREQUIREDDELIVERABLES  Navigation algorithm  Embedded system code for navigation algorithmESTIMATED One YearDURATIONSPONSORING WING R&IW Page 34 of 58
    • PROJECT TITLE Remote sensing of physical parametersOBJECTIVES To acquire data with time from different sensors from remote location and transmit them through serial link and plot them on GUI in real timePROJECT OUTLINE  Number of sensors: Minimum 20  Sampling rate: 100 Hz  Resolution: 12-bit  Distance b/w sensor and monitoring station: 500 meter on wire and 100 meter on RFMAJOR EQUIPMENT & Appropriate softwareSOFTWAREREQUIREDDELIVERABLES A GUI based system with real time data acquisition from different sensors in some remote locationsESTIMATED One YearDURATIONSPONSORING WING R&IW Page 35 of 58
    • PROJECT TITLE Stabilized Platform ControllerOBJECTIVES To design and develop Electro-Mechanical/Hydraulic System to stabilize the platformPROJECT OUTLINE  A mechanical system may be designed to realize the balance platform and mechanism to control it  Operating conditions like pressure, temperature, and humidity must be defined  Define operating ranges like maximum tilt angle, accuracy, resolution, precision, refresh rate, settling time  User friendly interface and control (GUI)  Load limits (Maximum mass and its mounting precautions like CG, center of mass, dimensions of payload to be fixed/ mounted on platform)  Operating voltage is 24~36 Volt DCMAJOR EQUIPMENT & Appropriate softwareSOFTWAREREQUIREDDELIVERABLES A stabilized platform capable of stabilizing itself for with in defined range of tilt angleESTIMATED One YearDURATIONSPONSORING WING R&IW Page 36 of 58
    • PROJECT TITLE Implementation of JPEG2000 Image Compression Software Using KAKADU_V2.2.3OBJECTIVES Software development for JPEG2000 Image Compression and DecompressionPROJECT OUTLINE  Study of Image Compression Techniques and MATLAB Image Compression Toolbox  Perform lossless image compression on image (Gray Scale/ Single Channel) and save the file into .jp2 standard.  In the next step the software would take .jp2 file as input and perform image decompression and display in the GUIMAJOR EQUIPMENT & Appropriate software, C++SOFTWAREREQUIREDDELIVERABLES GUI based comprehensive design software with proper display, image size, compression ratio, PSNR of image after compression/decompression, number of tiles, number of code blocks, type of filter usedESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 37 of 58
    • PROJECT TITLE Design and development of CPLD board for generation of timing signals for CCD sensorsOBJECTIVES It is required to design and Develop a CPLD board for clock signal generation up-to 10 MHzPROJECT OUTLINE  Study of CPLD  Familiarization with High speed PCB Design Software like Orcad, DXP Protel  Programming of CPLD  Design of PCB for Clock signal GenerationMAJOR EQUIPMENT & Orcad, DXP ProtelSOFTWAREREQUIREDDELIVERABLES The board should be capable of generating 10 different signals at 10 MHz outputESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 38 of 58
    • PROJECT TITLE Design and development of speed and position controlled platform for Linear Image SensorOBJECTIVES It is required to design and develop a speed and position controlled stable platform for mounting of Imaging sensorPROJECT OUTLINE  Study of Linear CCD Sensor  Study of Servo Motors  Development of Control Circuitry for Servo Motor  Design and Development of the Platform for Imaging SensorMAJOR EQUIPMENT & LabviewSOFTWAREREQUIREDDELIVERABLES  The platform should be capable to move smoothly at a speed of 2 mm/s to 20 mm/s and scan an area of 600mm.  Bi-directional control is requiredESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 39 of 58
    • PROJECT TITLE Design and development of high speed ADC moduleOBJECTIVES To design and develop a high speed ADC module for image acquisitionPROJECT OUTLINE  Study of Linear CCD Sensor  Study of High speed A/D techniques  Familiarization with Orcad or Protel DXP  Design of PCB for ADCMAJOR EQUIPMENT & Orcad, Protel DXPSOFTWAREREQUIREDDELIVERABLES The ADC should be able to convert analog output of sensor module to digital data @ 10 M Sample/sESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 40 of 58
    • PROJECT TITLE Design of a Schmidt Cassegrain telescopeOBJECTIVES Design of a Schmidt Cassegrain telescope by selecting and applying most efficient ray tracing technique and validation of the design using OSLOPROJECT OUTLINE  Study of various telescope designs and their application, mainly focusing on space telescopes  Selection of efficient ray tracing technique and design of optical layout accordingly  Familiarization with Optical design Software OSLO  Design of Optical telescope on softwareMAJOR EQUIPMENT & OSLOSOFTWAREREQUIREDDELIVERABLES Optical layout of telescope (OSLO or ZEMAX file)ESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 41 of 58
    • PROJECT TITLE Design of a Ritchey Chretien telescopeOBJECTIVES Design of a Ritchey Cretin telescope by selecting and applying most efficient ray tracing technique using OSLO. (Specifications will be provided)PROJECT OUTLINE  Study of various telescope designs and their application, mainly focusing on space telescopes.  Selection of efficient ray tracing technique and design of optical layout accordingly.  Familiarization with Optical design Software ZEMAX/ OSLO  Design of Optical telescope on softwareMAJOR EQUIPMENT & ZEMAX, OSLOSOFTWAREREQUIREDDELIVERABLES Optical layout of telescope (OSLO or ZEMAX file)ESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 42 of 58
    • PROJECT TITLE Power Management and Control System Microcontroller/ FPGA basedOBJECTIVES Design & Development of Microcontroller/FPGA based Power Management and Control SystemPROJECT OUTLINE  Study of Satellite Power System  Design of power management scheme  Simulation of management in Matlab  Development of code  Development of Hardware  Testing of developed systemMAJOR EQUIPMENT & MatlabSOFTWAREREQUIREDDELIVERABLES Simulations, coding and HardwareESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 43 of 58
    • PROJECT TITLE Variable Switching Power supply of 5-30volt output @ 6ampereOBJECTIVES Design & Development of Variable Switching Power supply of 5- 30volt output @ 6amperePROJECT OUTLINE  Study of switching regulators.  Simulation of switching supply  Development of Hardware and Software  Testing of developed systemMAJOR EQUIPMENT & Matlab, LabviewSOFTWAREREQUIREDDELIVERABLES Simulations , coding and HardwareESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 44 of 58
    • PROJECT TITLE DSP/FPGA implementation of Kalman filter based sensor fusion algorithm for attitude sensors (gyroscope, accelerometer/sun-sensor and magnetometer)OBJECTIVES The task incorporates the implementation of the attitude estimation algorithm (already developed) on a DSP/FPGA platform and optimizing its performancePROJECT OUTLINE  The students will be provided with the already developed MATLAB code and preliminary instructions on the hardware design.  They will use suitable DSP/ FPGA commercial-off-the-shelf (COTS) based technologies for system implementation.  MEMS based and COTS sensors will be used for the purposeMAJOR EQUIPMENT & MatlabSOFTWAREREQUIREDDELIVERABLES  Properly formatted code generation and optimization of the code for platform specific requirements.  Complete working hardware implementation for validating the implemented algorithmESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 45 of 58
    • PROJECT TITLE DSP/FPGA implementation of high fidelity orbit propagatorOBJECTIVES The task incorporates the implementation of the mentioned algorithm (already developed) on a DSP/FPGA platform and optimizing its performance according to the platformPROJECT OUTLINE  The students will be provided with the already developed MATLAB code and preliminary instructions on the hardware design.  They will use suitable DSP/ FPGA commercial-off-the-shelf (COTS) based technologies for system implementationMAJOR EQUIPMENT & MatlabSOFTWAREREQUIREDDELIVERABLES Properly formatted code generation and optimization of the code for platform specific requirementsESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 46 of 58
    • PROJECT TITLE Analysis of space and time (memory and processing) complexities of different pattern matching algorithms for star identificationOBJECTIVES The task is to analyze the spatial and temporal complexities of pattern matching algorithms and to extend or modify them for optimization of star identification algorithm (already implemented) for star trackerPROJECT OUTLINE  The students will be provided with the already developed star identification algorithm and the star catalogue as well as with the precise details of working mechanism of star tracker for attitude determination  They will explore and analyze the different available algorithms for their temporal and spatial complexities and will optimize the best amongst themMAJOR EQUIPMENT & Appropriate SoftwareSOFTWAREREQUIREDDELIVERABLES Comparison of results achieved through different algorithms. Optimal star identification algorithmESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 47 of 58
    • PROJECT TITLE PCB Analysis of Vertex-V FPGA Board using HYPERLYNX 7.7OBJECTIVES PCB ANALYSIS OF VERTEX-V FPGA BOARD using HYPERLYNX 7.7PROJECT OUTLINE  EMI EMC Analysis using Hyper lynx Software  Pre-Layout Analysis  DDR2 to FPGA Route estimation with optimized S-Parameters  PCIE to FPGA Route estimation with optimized S-Parameters and route length  High Speed I/O connector to FPGA Route estimation with optimized S-Parameter and route Length  Identification of Stackup Layers and arrangement of power layersMAJOR EQUIPMENT & Matlab, LabviewSOFTWAREREQUIREDDELIVERABLES A report of S-parameters and SI analysis of FPGA Based boardESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 48 of 58
    • PROJECT TITLE JTAG TAP Controller for Satellite On-board Configuration Monitoring and Control for Reliable System ImplementationOBJECTIVES To design and develop JTAG Test Access Point (TAP) Control System that detects the devices attached to the JTAG chain and reads the device identification through a MicrocontrollerPROJECT OUTLINE  Study IEEE1149.1 JTAG Protocol  Study of JTAG Tool Chaining for Multiple device access  Implementation of Design in Microcontroller  Interfacing the Microcontroller to the target board through JTAG  Interfacing the Microcontroller to PC through serial port for display of device ID and statusMAJOR EQUIPMENT & LabviewSOFTWAREREQUIREDDELIVERABLES Source Code, Design Files, Hardware Demonstration, Implementation and Design DocumentsESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 49 of 58
    • PROJECT TITLE CCSDS based Packet Data extraction software of Remote Sensing Satellite Image DataOBJECTIVES To Design & Develop GUI based Software that will extract data from incoming packets of Imaging SatellitePROJECT OUTLINE  To extract data from data fields of incoming packets  Packets will be consist of pre-define format  Pre-define format include sizes of headers and its sub-fields, data field length and their complete specification will be provided by SUPARCO  Packets will be consist of either valid data or idle data identified through its header field  Data from valid packets will be extracted and discarded if idle packet  Generate and save text Files of extracted information  Keep Record of number of packets arrived, lost packets, missing data, number of valid and idle packets  GUI Development  Text file contains raw data of specified packet format will be given by SUPARCO. Also, detailed specification of Packet format will be providedMAJOR EQUIPMENT & Matlab , Visual C or otherSOFTWAREREQUIREDDELIVERABLES  GUI Software developed on above mentioned software  Complete Source Code Project ReportESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 50 of 58
    • PROJECT TITLE Design and Development of CCSDS based Concatenated Reed Solomon Decoder & Viterbi Decoder along with de- Interleaver SoftwareOBJECTIVES To design and develop concatenated de-coding scheme based on Reed-Solomon Decoder(255,223) & Viterbi Decoder software along with de-Interleaver of depth I=5PROJECT OUTLINE • Study of Reed Solomon Encoder & Decoder • Study of Convolution Coding & Viterbi Decoder • Study of Interleaving and De-Interleaving • Algorithm Design of Reed Solomon Decoder • Algorithm Design of Viterbi Decoder • Algorithm Design De-Interleaver • Design implementation on VB, C or any high level languageMAJOR EQUIPMENT & VB, CSOFTWAREREQUIREDDELIVERABLES • Source Code • Design ReportESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 51 of 58
    • PROJECT TITLE Study of Reliable System Design Techniques like ( Triple Modular Redundancy (TMR)) for increasing the reliability of Embedded System in SpaceOBJECTIVES Case Study for the Triple Modular Scheme for Commercial grade Processor (PowerPC, intel) to increase the system reliability/Availability for Space applicationsPROJECT OUTLINE • Study different Reliability techniques • Study of Space Environment and Reliability Hazards like (out- gasing, Radiation effects) • Study of Single Event Latch Up and Single Event Failure Proposed Design for Space application using TMR schemeMAJOR EQUIPMENT & N/ASOFTWAREREQUIREDDELIVERABLES Study ReportESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 52 of 58
    • PROJECT TITLE Design of Triple Modular Redundancy (TMR) based scheme for PowerPC based Payload System incorporating DDR2 memory and FPGA based Endpoint Devices for LEO satelliteOBJECTIVES To design an efficient and reliable Payload System for LEO Satellite based on a high speed processor, memory and bus interfacePROJECT OUTLINE • Study different Reliability techniques used in embedded systems particularly those related to Space applications • Study of Space Environment and Reliability Hazards like (out- gasing, Radiation effects, SEU, SEL) • Proposed Design for Space application using TMR schemeMAJOR EQUIPMENT & Appropriate SoftwareSOFTWAREREQUIREDDELIVERABLES Implementable TMR scheme including any source code(s), design files and simulation filesESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 53 of 58
    • PROJECT TITLE Study of EDAC(Error Detection and correction) Scheme for DDR memory for space applicationOBJECTIVES Case Study for the Error detection and correction schemes for memory device with special focus on DDR memoryPROJECT OUTLINE • Study different Error Detection and Error Controlling techniques • Study of Errors occur in memory read/write transactions • Proposed Design for Robust EDAC controller for DDR memoryMAJOR EQUIPMENT & MatlabSOFTWAREREQUIREDDELIVERABLES Study ReportESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 54 of 58
    • PROJECT TITLE Analysis of space and time (memory and processing) complexities of different pattern matching algorithms for star identificationOBJECTIVES The task is to analyze the spatial and temporal complexities of pattern matching algorithms and to extend or modify them for optimization of star identification algorithm (already implemented) for star trackerPROJECT OUTLINE • The students will be provided with the already developed star identification algorithm and the star catalogue as well as with the precise details of working mechanism of star tracker for attitude determination. • They will explore and analyze the different available algorithms for their temporal and spatial complexities and will optimize the best amongst themMAJOR EQUIPMENT & Appropriate Software, any high-level languageSOFTWAREREQUIREDDELIVERABLES Comparison of results achieved through different algorithms. Optimal star identification algorithmESTIMATED One YearDURATIONSPONSORING WING Space Electronics Page 55 of 58
    • PROJECT TITLE Wind Resistant Stability of Tubular Wind Turbine TowersOBJECTIVES To study the stability criteria for Tubular Towers of Wind Turbine under wind loadingPROJECT OUTLINE • Literature review • Optimization of basic material properties • Structural configuration (base diameter, top diameter, taper ratio, thickness of material etc.) of tubular tower and their dependence on height of the tower • Finite Element Analysis (Static, dynamic and buckling) of different configurations • Report writing & presentationMAJOR EQUIPMENT & AnsysSOFTWAREREQUIREDDELIVERABLES • Optimized material properties • Parametric study of structural configuration • Report writing & presentationESTIMATED One YearDURATIONSPONSORING WING Space Technology Page 56 of 58
    • PROJECT TITLE Manufacturing and Assembling of Tubular Towers of Wind TurbineOBJECTIVES To study the different scenarios of manufacturing and assembling Tubular Towers of Wind TurbinePROJECT OUTLINE • Literature review • Rolling of sheets • Flanges • Welding • AssemblingMAJOR EQUIPMENT & AnsysSOFTWAREREQUIREDDELIVERABLES • Tapered rolling procedures • Welding procedure and characterization of weld properties • Design of welding jigs to control weld distortions • Flanges and their joints with tower • Procedure for assembling of tubular towerESTIMATED One YearDURATIONSPONSORING WING Space Technology Page 57 of 58
    • PROJECT TITLE To Study Flow Characteristics around Straight and Curved Fin ProjectilesOBJECTIVES To study flow anomalies in curved fin projectilesPROJECT OUTLINE • Literature Review • CFD analysis of straight and curved fin projectile • Grid independence study • Validation of CFD results with available experimental data • Detail study of anomalies in curved fin projectileMAJOR EQUIPMENT & Standard CFD softwareSOFTWAREREQUIREDDELIVERABLES • Solid model, grid, and solution files of all configurations • ReportESTIMATED One YearDURATIONSPONSORING WING Space Technology Page 58 of 58