一种四旋翼无人机通控一体轨迹设计框架和优化方法
By constructing a discretized spatiotemporal model and a dual-loop control architecture for an unmanned aerial vehicle (UAV) air-to-ground communication system, and combining the principles of rigid body dynamics, the coupling relationship between the flight dynamics of the rotary-wing UAV and the communication antenna is optimized. This solves the problems of model mismatch and wasted attitude degrees of freedom in existing technologies, and achieves more efficient communication performance.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- NANTONG UNIV
- Filing Date
- 2026-03-04
- Publication Date
- 2026-07-17
AI Technical Summary
Existing UAV trajectory optimization techniques ignore the underactuated characteristics of rotorcraft UAVs and the strong coupling of antenna attitude, resulting in model mismatch, wasted attitude degrees of freedom, and physical infeasibility, which affects communication performance.
A discretized spatiotemporal model of an UAV air-to-ground communication system is constructed. Combining a dual-loop control architecture and rigid body dynamics principles, the coupling relationship between the UAV's flight dynamics and the communication antenna is optimized. The trajectory is optimized using sequential convex approximation and semi-definite relaxation algorithms, and the attitude control antenna beam is actively utilized.
This approach achieves tight coupling between UAV flight dynamics and communication antennas, improving the transmission rate and coverage performance of the communication system, avoiding the mismatch between theory and practice, and providing an efficient optimization solution.
Smart Images
Figure CN122411490A_ABST