Technical Description
This invention introduces a multi-rotor UAV that achieves attitude and position control by dynamically shifting its Center of Gravity (CoG) through movable landing gear. By manipulating control masses on foldable legs, the vehicle reduces reliance on traditional rotor speed variations for maneuvering.
Problems Addressed
- Inadequate Actuator Robustness
- Low Flight Endurance
- Inefficient Disturbance Rejection
- Limited Large-Scale Agility
- Unstable Ground Effects
- Suboptimal Load Handling
Tech Features
- Foldable Landing Gear
- Moveable Control Masses
- Pivotable Drive Motors
- Integral Backstepping Control
- Ground Effect Mitigation
- Variable CoG Maneuvering
Target Audience
- Defense and Surveillance
- Logistics and Delivery
- Emergency Response
- Precision Agriculture
- Research & Development
Tech ID: P04-1948 TRL 5 Patent Status: Granted Available For Exclusive and Non-exclusive License
