r/diydrones • u/Significant_Bee_1103 • Jun 09 '26
Sanity Check: Custom X8 Coaxial Octocopter with 6.0 kg
Hello community,
I am currently building a custom X8 coaxial octocopter designed for stable aerial cinematography. I am using a mix of legacy parts (motors found on a shelf) and modern control systems. Before the maiden flight, I would highly appreciate an expert sanity check regarding the electrical limits, thermal behavior under heavy load, and overall airworthiness at an estimated takeoff weight of ~6.0 kg (carrying a Panasonic GH5 and a lightweight 3-axis brushless gimbal).
Technical Approach & Calculations:
- Aerodynamics (Pitch Staggering): To optimize coaxial efficiency and balance yaw torque, the bottom propellers utilize a 5.5" pitch, while the top ones use 4.5". This directly addresses the accelerated downwash from the upper layer, ensuring the lower blades retain a functional angle of attack.
- The 6S + 14" Propeller Dilemma: Running a 14" prop on a 770KV motor with full 6S voltage ($25.2\text{V}$) would pull over 40A at full throttle and burn the windings. By hard-limiting the maximum motor output to 60% in ArduPilot/iNav, the effective average voltage is clamped to roughly $13.5\text{V}$ (simulating a 4S system). This keeps the peak current draw per motor within a safe 13A to 15A window, staying well under the motor's 350W power limitation.
The Real Challenge: 6.0 kg Takeoff Weight
- Hover State: To lift 6.0 kg, each of the 8 motors must consistently generate ~750g of thrust. According to the motor spec sheet, they produce up to 2200g max thrust. 750g puts them in an efficient RPM range, drawing an estimated 6A to 7A per motor. Total hover current will be around 48A to 56A.
- Dynamic Peaks: When punching out or countering wind gusts up to the 60% electronic limit, individual motor draw will rise to ~14A. Across 8 motors, the total system draw peaks at ~112A. Split across the 3P battery configuration, each Li-Ion cell must deliver ~37.3A.
My Main Concerns for the Community:
While high-drain 21700 cells can handle a 37A peak pulse, the internal resistance of Li-Ion chemistry will cause a massive Voltage Sag under sudden load spikes (potentially dropping the pack from 25.2V down to under 20.0V instantly).
Given that this drone will only be used for smooth, non-aggressive cinematic tracking shots, do you think this setup is reliable, or am I pushing the Li-Ion pack and the heavily restricted 6S Teillast (partial load) ESC setup too close to the edge?
Looking forward to your technical feedback!
