Competition | 2023-2024 Aerial Evolution of Canada Student Competition | ||||||
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Team | Waterloo Aerial Robotics Group | ||||||
Technical Director | |||||||
Version | Document Version
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On this page |
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Airframe | |||||||||||||||||||
Part Function | Manufacturer | Part Name & Link | Qty | Notes | |||||||||||||||
Propulsion | |||||||||||||||||||
Part Function | Manufacturer | Part Name & Link | Qty | Notes | |||||||||||||||
Propellers | T-Motor | MF2211 | 4 Indiv 2 CW 2 CCW |
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Motors | T-Motor | Antigravity MN6007II | 4 Indiv | See Motor Selection Subpage | |||||||||||||||
ESC | Advanced Power Drives [APD] | 120F3[X]v2 | 4 |
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Power Distribution | |||||||||||||||||||
Part Function | Manufacturer | Part Name & Link | Qty | Notes | |||||||||||||||
Batteries | Turnigy | Heavy Duty 5000mAh 6s 60C LiPo Pack w/XT90 | 4-6 |
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PDB | Advanced Power Drives [APD] | PDB500[X] | 1 |
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Power Monitor | Holybro | Holybro PM02D High Voltage | 1 | ||||||||||||||||
BEC | Mateksys | BEC12s-Pro | 1-2 |
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Flight Control System | |||||||||||||||||||
Part Function | Manufacturer | Part Name & Link | Qty | Notes | |||||||||||||||
Autopilot | Holybro | Pixhawk 5/6x + SD Card (logging) | 1 |
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GPS | Holybro | Holybro M9/10N GPS | 1 Prim 1 Sec |
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Unknown | Future RTK system |
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Rangefinder 🔍 | Benewake | TFMINI-S Micro LIDAR Module I2C | 1+ |
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Optical Flow Sensor (OFS) 🔍 | CubePilot | HereFlow | 1 |
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Compass 📉 | |||||||||||||||||||
Barometer 📉 | |||||||||||||||||||
Autonomy computer | NVIDIA Connect Tech | Jetson TX2i with Quasar carrier | 1 | Is not mounted on the drone. Alternatively: Any computer that supports real time image inference at the required rate. | |||||||||||||||
Raspberry Pi | |||||||||||||||||||
Omnidirectional Lidar | Lightware | SF 45/B | |||||||||||||||||
Ground station computer | Lenovo | Lenovo ThinkPad T490 | 1 | Alternatively: Any computer that supports Mission Planner. | |||||||||||||||
RF + Peripherals (grouped because it’s small bits of things) | |||||||||||||||||||
Part Function | Manufacturer | Part Name & Link | Qty | Notes | |||||||||||||||
Control Link | TBD | ELRS Diversity RX | 1 | 1 of either | |||||||||||||||
WARG | ELRS Gemini | 1 | |||||||||||||||||
Telemetry Link | 1 | 1 of Either Potentially double up 4 redundancy | |||||||||||||||||
Abra Electronics | LTE Hat | ||||||||||||||||||
RF Design | RFD900x | ||||||||||||||||||
Video Transmitter | Mateksys | VTX 1G3SE | 1 of either |
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Foxeer | 1.2G 5W (Enhanced) 4ch | ||||||||||||||||||
FPV Cameras | Caddx | Baby Ratel 2 | 2 | ||||||||||||||||
OSD | Holybro | Holybro Micro OSD V2 | 1 |
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Video Mux | Lumenier | 3-Way Multi Camera Video Switcher Board | 1 | ||||||||||||||||
Lighting 🔍 | - | - | NAVLights | ||||||||||||||||
- | - | Landing Lights | |||||||||||||||||
CV Camera | Hupuu | $200 CV Camera | 1 | ||||||||||||||||
Groundside | |||||||||||||||||||
Part Function | Manufacturer | Part Name & Link | Qty | Notes | |||||||||||||||
Groundstation LaptopGround station computer | Lenovo | Thinkpad T490? | 1 | Alternatively: Any computer that can run Mission Planner. | |||||||||||||||
1.3G Video RX | ReadyMade RC | 900-1.3 GHz Receiver w/Tuner | 1 | ||||||||||||||||
5.8G Video TX | AKK | TS832 5.8 GHz VTX | 1 | ||||||||||||||||
RC Control Link | WARG | ELRS Gemini | 1 | PREF GEMINI WHEN POSSIBLE | |||||||||||||||
RadioMaster | RadioMaster Ranger FCC | 1 | |||||||||||||||||
Telemetry Link | WARG | ELRS Gemini | 1 | Used with flow control RC + MAVLink simultaneously. RC Priority. Backup to LTE. | |||||||||||||||
RFDesign | RFD900x | 1 | Only used as a backup option. Not to be mounted regularly. | ||||||||||||||||
❓ | LTE Hotspot | 1 | No manufacturer | ||||||||||||||||
Telemetry Relay | Xbee | XBEE Pro 5.8 | 2 | Primary Telem relay | |||||||||||||||
ELRS | ELRS Airport | Backup. Not to be mounted normally. | |||||||||||||||||
FPV Goggles | - | Pilot Preference | |||||||||||||||||
RC Controller | RadioMaster | TX16s MkII ELRS Mode 2 HALL | 2 |
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Video Monitor | - | Generic 5.8 GHz Receiver | |||||||||||||||||
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Min | Recc/Avg | Max | |
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Propeller Diameter (in) | 20 | 22 | 24 |
Battery Voltage (v) | 36 | - | 50.4 |
Takeoff Weight | 4.5 | < | 8 |
Thrust (kg) | ~16 | ||
Flight time (min) | 30 | TBD (40?) | |
Wind Lim. (kt) | < 20 | TBD (< 60) | |
Altitude (m) | < 120 | 200 | |
Horizontal Pos Accuracy (cm) | +/- 2 | +/-30 | +/- 200 |
Vertical Pos Accuracy (cm) | +/- 2 | +/- 15 | +/- 30 |
Usable Range (km) | 1 | 10 | inf w/LTE |
Airframe
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Pegasus is an X-frame configuration and motor arms attached directly to a straight aluminum block. Here are some of the key notes:
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Most components will run ~ 20-30 degrees hotter than ambient, and will thermal limit around 80 degrees celcius. This means that on an average “warm” day, our components have around 20-30 degrees of headroom. Think about how much hotter a cabin may cause components to be, especially if black carbon fiber and in the air (exposed, not under shade).
Propulsion
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Panel | ||||||||
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Electrical, please insert a schematic & layout diagram with motors, connectors, esc’s with breaks to the rest of the HV distribution system |
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Anti-spark XT90s need to be used for our battery connections. Anti-Spark Connector Standards
Power Distribution
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On Pegasus, “power distribution” refers to all elements that affect and interact with power before it is distributed to individual components. Typically, this includes:
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DShot is only available on FMU out as of 4.4.0, but will be available (tentatively), on certain I/O FMU Outputs in the future.
Flight Control System
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Pegasus will operate using an ardupilot software stack. As of Fall 2023 Pegasus runs software revision 4.4.0, as this brings necessary changes for digital power monitoring and bidirectional dshot.
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Ground station is at the cruise scope, for multiple waypoints, and is responsible for guiding the drone along the most efficient waypoint to waypoint path. Control is handled by the pathing system and Mission Planner running on the ground station computer.
RF + Peripherals
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There are a number of external devices on the drone. Autonomy is largely responsible for additional compute, while Electrical is largely responsible for RF
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