1. Terrestrial command and control center | 2. Obstacle avoidance technology for drones | 3. Wing Form | 4. Takeoff / Landing technology | 5. Engine | 6. Power source |
---|---|---|---|---|---|
Command and control using Dynamic Data-Driven Application System (DDDAS) | using potential fields | Fixed wing | Vertically | Electric | Fuel tanks |
Dynamic model using frequency-domain system identification techniques | Obstacle avoidance algorithm based on the fluid mechanics panel methods | Rotary wing | With a runway | Piston | Batteries and Accus |
H-infinity loop-shaping technique | using dynamic window approach | Tilt wing | Hybrid technology | Rotary | Fuel cells |
Linear quadratic (LQ) design methods | Vision (optical flow)-based obstacle avoidance | Hybrid form | Alternative | Turbo-prop | Photovoltaic |
L1 adaptive control | Turbo-jet/fan | Nuclear | |||
Neural network based adaptive flight controller |