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Avionics
FAR/MARS
System Overview
Avionics System Subsections:
- Flight Computer
- Analog Control System
- Relay Station
- REDS
- Harness
- Software (Data Viz)
Mounting
Flight
Computer
Analog Control System
● All bunker commands will be sent using the ACS
● Device consists of:
○ Custom PCB
○ Raspberry Pi
○ Arduino
○ 7V DC power supply
○ 14 toggle switches
○ 1 abort button
○ 3 safety switches
○ 2 display screens
○ 15 state LEDs
○ 1 volt meter
Analog Control System
● Designed to be highly configurable/easy
to access
● Three removable plates
1. Display plate
2. Back plate
3. Front plate
● All components interior to ACS will sit
on a removable acrylic plate
1
2
3
Analog Control System Layout
1
2
3
5
1. Display
2. Toggle Switch
3. LED Indicator
4. Abort Button
5. Key Switch
4
Analog Control System PCB
● Printed Circuit Board Design
○ 3 different versions
1. KiCAD
2. Altium v.1
3. Altium v.2
○ Relays are actively grounded
○ Switch needs to be placed
between signal and ground
○ PCB manufacturing choice:
OshPark
○ JST connectors for I/O pins
○ Ethernet connectors for long
distance signal transmission
KiCAD
Altium v.1
Latest Version:
“Altium V.2”
Analog Control System PCB
Ethernet 2 pin JST
Purpose: Organize ACS
interior circuit so that it
is both easily
replaceable and reliable
Switch connectors
LED connectors
int LOX = 12;
int CH4 = 11;
int IGNITION = 10;
int LOX_s = 7;
int CH4_s = 6;
int LAUNCH_s = 5;
int vLOX;
int vCH4;
int vLAUNCH;
void setup(){
pinMode(LOX, OUTPUT);
pinMode(CH4, OUTPUT);
pinMode(IGNITION, OUTPUT);
pinMode(LOX_s, INPUT);
pinMode(CH4_s, INPUT);
pinMode(LAUNCH_s, INPUT);
digitalWrite(LOX, HIGH);
digitalWrite(CH4, HIGH);
digitalWrite(IGNITION, HIGH);
}
void loop(){
vLAUNCH =
digitalRead(LAUNCH_s);
vLOX = digitalRead(LOX_s);
vCH4 = digitalRead(CH4_s);
MPV and Spark Ignition Relays
Simple Arduino code to turn on ignitor and actuate valves with time delay
if (vLAUNCH == HIGH) {
digitalWrite(IGNITION, LOW);
delay(1000);
digitalWrite(CH4, LOW);
delay(250);
digitalWrite(LOX, LOW);
}
if (vLOX == HIGH) {
digitalWrite(LOX, LOW);
}
if (vCH4 == HIGH) {
digitalWrite(CH4, LOW);
}
else {
digitalWrite(LOX, HIGH);
digitalWrite(CH4, HIGH);
digitalWrite(IGNITION, HIGH);
}
}
Relay Station Circuit Diagram
4 step safety routine:
AC Power Switch, Safety Switch, Safety Relay, ACS Key Switch
Relay Station Pelican Case
iM2370 Storm Case
● Interior: 18.20" × 12.10" × 5.20"
● Watertight, crushproof, and dustproof
● Two Press & Pull Latches
● Two Padlockable Hasps
● Double-layered, Soft-grip Handle
Relay Station CAD
DIN rail connectors
3 pin bulkheads
Raspberry Pi
Ethernet bulkheads
Relays
Power supply
bulkhead 24VDC supply
Relay Station PCB
Pelican case
REDS
Rocket Emergency Depressurization System
In the shared valve scenario, there needs to be a seperate connector into the
rocket specifically for REDS. Vent valve lead wires will be spliced in boat tail
area and attached to both the Umbilical and REDS connectors. This will be done
using a simple PCB with inline diodes attached to the REDS connector and a
simple passthrough for the Umbilical connector.
REDS (P1)
connector
Altium
Harness Connections to Rocket
Specs:
● 13A capacity
● 12 pins
● Dimensions: ½” by ½”
● McMaster: 6168T79
Pinout:
1&2: LOX VENT
3&4: CH4 VENT
5&6: DATA
7&8: LOX MPV
9&10: CH4 MPV
11&12: AUX
Harness Overall Structure
1: Connection to exterior. 12 pin connector, 10 currently populated
2: VV leads split off to REDS connector, MPVs connected to initiators, fill solenoids connected
3: CH4 Vent splits off main line.
4: LOX Vent splits off
5: Data lines terminate at board
Lox Tank Passthrough CH4 Tank Passthrough
2 data wire = 0.132” diameter
+
2 Lox Vent wire = 2*0.132”
~0.4” diameter total
2 data wire = 0.132” diameter
+
2 Lox Vent wire = 2*0.312 =
0.264”
+
2 CH4 Vent wire = 2*0.132”
0.264
~0.66” diameter total
Helium Tank Passthrough
LOX Tank Passthrough
CH4 Tank Passthrough
Relay Station:
● Relay max current: 10A
● Power source max current: 5A
● Solenoid max current draw: 0.1A x 5
● Clark Cooper vent valves: 1A x 2
Max current draw: ~2.5A
Analog Control System:
● Relay activation current: 70 mA x 12
● Diode activation current: 30 mA x 12
● Power source max current: 2A
Max current draw: ~1.2A
Power Constraints
Ignitor System:
● Spark ignitor max current: 4A
● Power source max current: 6A
Max current draw: ~4A
Software
QtDesigner:
GUI Rapid Application Development tool for the Qt GUI toolkit
Software will display:
● Helium system
pressures
● Rocket tank pressures
● Overpressure warnings
● Breakwire read
● IMU data
● Tank weight
Software
*Test Stand PyQt Example

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FAR/MARS Avionics CDR

  • 2. System Overview Avionics System Subsections: - Flight Computer - Analog Control System - Relay Station - REDS - Harness - Software (Data Viz)
  • 4. Analog Control System ● All bunker commands will be sent using the ACS ● Device consists of: ○ Custom PCB ○ Raspberry Pi ○ Arduino ○ 7V DC power supply ○ 14 toggle switches ○ 1 abort button ○ 3 safety switches ○ 2 display screens ○ 15 state LEDs ○ 1 volt meter
  • 5. Analog Control System ● Designed to be highly configurable/easy to access ● Three removable plates 1. Display plate 2. Back plate 3. Front plate ● All components interior to ACS will sit on a removable acrylic plate 1 2 3
  • 6. Analog Control System Layout 1 2 3 5 1. Display 2. Toggle Switch 3. LED Indicator 4. Abort Button 5. Key Switch 4
  • 7. Analog Control System PCB ● Printed Circuit Board Design ○ 3 different versions 1. KiCAD 2. Altium v.1 3. Altium v.2 ○ Relays are actively grounded ○ Switch needs to be placed between signal and ground ○ PCB manufacturing choice: OshPark ○ JST connectors for I/O pins ○ Ethernet connectors for long distance signal transmission KiCAD Altium v.1
  • 9. Analog Control System PCB Ethernet 2 pin JST Purpose: Organize ACS interior circuit so that it is both easily replaceable and reliable Switch connectors LED connectors
  • 10. int LOX = 12; int CH4 = 11; int IGNITION = 10; int LOX_s = 7; int CH4_s = 6; int LAUNCH_s = 5; int vLOX; int vCH4; int vLAUNCH; void setup(){ pinMode(LOX, OUTPUT); pinMode(CH4, OUTPUT); pinMode(IGNITION, OUTPUT); pinMode(LOX_s, INPUT); pinMode(CH4_s, INPUT); pinMode(LAUNCH_s, INPUT); digitalWrite(LOX, HIGH); digitalWrite(CH4, HIGH); digitalWrite(IGNITION, HIGH); } void loop(){ vLAUNCH = digitalRead(LAUNCH_s); vLOX = digitalRead(LOX_s); vCH4 = digitalRead(CH4_s); MPV and Spark Ignition Relays Simple Arduino code to turn on ignitor and actuate valves with time delay if (vLAUNCH == HIGH) { digitalWrite(IGNITION, LOW); delay(1000); digitalWrite(CH4, LOW); delay(250); digitalWrite(LOX, LOW); } if (vLOX == HIGH) { digitalWrite(LOX, LOW); } if (vCH4 == HIGH) { digitalWrite(CH4, LOW); } else { digitalWrite(LOX, HIGH); digitalWrite(CH4, HIGH); digitalWrite(IGNITION, HIGH); } }
  • 11. Relay Station Circuit Diagram 4 step safety routine: AC Power Switch, Safety Switch, Safety Relay, ACS Key Switch
  • 12. Relay Station Pelican Case iM2370 Storm Case ● Interior: 18.20" × 12.10" × 5.20" ● Watertight, crushproof, and dustproof ● Two Press & Pull Latches ● Two Padlockable Hasps ● Double-layered, Soft-grip Handle
  • 13. Relay Station CAD DIN rail connectors 3 pin bulkheads Raspberry Pi Ethernet bulkheads Relays Power supply bulkhead 24VDC supply Relay Station PCB Pelican case
  • 14. REDS Rocket Emergency Depressurization System In the shared valve scenario, there needs to be a seperate connector into the rocket specifically for REDS. Vent valve lead wires will be spliced in boat tail area and attached to both the Umbilical and REDS connectors. This will be done using a simple PCB with inline diodes attached to the REDS connector and a simple passthrough for the Umbilical connector. REDS (P1) connector Altium
  • 15. Harness Connections to Rocket Specs: ● 13A capacity ● 12 pins ● Dimensions: ½” by ½” ● McMaster: 6168T79 Pinout: 1&2: LOX VENT 3&4: CH4 VENT 5&6: DATA 7&8: LOX MPV 9&10: CH4 MPV 11&12: AUX
  • 16. Harness Overall Structure 1: Connection to exterior. 12 pin connector, 10 currently populated 2: VV leads split off to REDS connector, MPVs connected to initiators, fill solenoids connected 3: CH4 Vent splits off main line. 4: LOX Vent splits off 5: Data lines terminate at board Lox Tank Passthrough CH4 Tank Passthrough 2 data wire = 0.132” diameter + 2 Lox Vent wire = 2*0.132” ~0.4” diameter total 2 data wire = 0.132” diameter + 2 Lox Vent wire = 2*0.312 = 0.264” + 2 CH4 Vent wire = 2*0.132” 0.264 ~0.66” diameter total
  • 20. Relay Station: ● Relay max current: 10A ● Power source max current: 5A ● Solenoid max current draw: 0.1A x 5 ● Clark Cooper vent valves: 1A x 2 Max current draw: ~2.5A Analog Control System: ● Relay activation current: 70 mA x 12 ● Diode activation current: 30 mA x 12 ● Power source max current: 2A Max current draw: ~1.2A Power Constraints Ignitor System: ● Spark ignitor max current: 4A ● Power source max current: 6A Max current draw: ~4A
  • 21. Software QtDesigner: GUI Rapid Application Development tool for the Qt GUI toolkit
  • 22. Software will display: ● Helium system pressures ● Rocket tank pressures ● Overpressure warnings ● Breakwire read ● IMU data ● Tank weight Software *Test Stand PyQt Example

Editor's Notes

  1. Cade Walton
  2. Cade Walton
  3. Cade Walton
  4. Cade Walton