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Drone (UAV): Theoretical Design and Analysis — Ep 01
Session 5
- Episode
- 01
- Run Time
- 1h 16s
- Published
- Oct 26, 2025
- Topic
- Drone (UAV)
- Course Progress
- 0%
About This Episode
Weight Estimation: Empty, Payload, Fuel/Battery.
The Master Equation: W₀ = Wₛtructure + Wₚayload + Wₑnergy.
Estimating Wing Loading (W/S) from stall, climb, cruise.
Estimating Thrust-to-Weight (T/W) from climb and cruise.