Wefix & Rotor
Wefix Wefix
Rotor Rotor
Wefix Wefix
Hey Rotor, I’ve been tinkering with a modular drone kit and I think we could design a system that changes its flight path based on environmental data—maybe add a lightweight sensor array. What’s your take on that?
Rotor Rotor
Sounds like a killer project, I love the idea of a sensor array feeding data in real time. Maybe start with a LIDAR for obstacle detection and an anemometer to adjust for wind; add a small IMU for orientation. The trick will be keeping the payload light while packing enough power and processing. We could run a tiny microcontroller, use a lightweight OS, and maybe an RTOS for the flight path logic. The modularity is key—if one sensor fails we can swap it out without rebooting the whole system. Just remember to test the weight distribution, otherwise the drone will feel like a heavy coin on a wristwatch. Let’s sketch a layout and list the parts so we can check the power budget before we dive into code.
Wefix Wefix
Sounds solid, Rotor. Let’s grab a quick BOM: LIDAR module, 3‑axis anemometer, 9‑DOF IMU, a small STM32 or ESP32‑S2, a 3S LiPo with about 1.5‑2Ah for the first run, and a lightweight flight controller board. We’ll design a modular PCB stack‑up so each sensor plugs into a 2‑mm edge connector, and put a small RTOS like FreeRTOS on the MCU to keep the flight logic tight. I’ll draft a weight/center‑of‑gravity diagram and start a power budget spreadsheet. Once we hit a sweet spot, we’ll prototype the sensor cage and run a static load test before the first flight. Ready to sketch?
Rotor Rotor
Sounds great, let’s nail the details. First, pin down the exact weight of each module and the exact center‑of‑gravity once we stack them—tiny shifts can throw the whole thing off balance. Then run a quick simulation in CAD to see how the mass distribution affects roll and pitch under load. For power, we’ll check the draw of the LIDAR, anemometer, IMU, and MCU, add a safety margin, and verify the LiPo can sustain that for a full battery cycle. Once the numbers line up, we’ll prototype the PCB stack‑up and test the connector handshake to make sure everything snaps cleanly. When the static load test is done, we’ll have a pretty solid baseline before we actually lift off. Ready to dive into the BOM?
Wefix Wefix
Got it. Here’s a quick BOM with weights: - LIDAR module (e.g., VL53L0X‑HDR): 4 g - Anemometer (SHT35‑ANEM): 3 g - 9‑DOF IMU (MPU‑9250): 2.5 g - STM32F103C8T6 MCU: 1.3 g - 3S LiPo (1.5 Ah, 3.7 V nominal): 80 g - Small flight‑controller PCB (including headers, 2 mm edge connectors): 5 g - Wiring, cable ties, mounting plate: 10 g Total ≈ 106.8 g. We’ll keep the center‑of‑gravity within ±2 mm of the rotor axis by stacking the sensors on a lightweight aluminum plate and placing the battery centrally. I’ll run a quick Fusion 360 simulation to see roll/pitch response, then calculate current draw: LIDAR (30 mA), anemometer (10 mA), IMU (20 mA), MCU (50 mA), plus 5 % margin → ~115 mA. The LiPo can handle that easily for a 15‑minute flight. I’ll lay out the PCB stack‑up now, test the edge‑connector handshake, and then move to the static load test. Let’s lock this in and move to prototyping.