CONTROL AND STABILIZATION OF A FLIGHT VEHICLE FROM A DETECTED PERTURBATION BY TILT AND ROTATION专利检索- 能垂直起飞或着陆的飞机专利检索查询-专利查询网

CONTROL AND STABILIZATION OF A FLIGHT VEHICLE FROM A DETECTED PERTURBATION BY TILT AND ROTATION
申请号	US15935689	申请日	2018-03-26	公开(公告)号	US20180284814A1	公开(公告)日	2018-10-04
申请人	Thomas A. Youmans;			发明人	Thomas A. Youmans;
摘要	A flight vehicle control and stabilization process detects and measures an orientation of a non-fixed portion relative to a fixed frame or portion of a flight vehicle, following a perturbation in the non-fixed portion from one or both of tilt and rotation thereof. A pilot or rider tilts or rotates the non-fixed portion, or both, to intentionally adjust the orientation and effect a change in the flight vehicle's direction. The flight vehicle control and stabilization process calculates a directional adjustment of the rest of the flight vehicle from this perturbation and induces the fixed portion to re-orient itself with the non-fixed portion to effect control and stability of the flight vehicle. The flight vehicle control and stabilization process also detects changes in speed and altitude, and includes stabilization components to adjust flight vehicle operation from unintentional payload movement on the non-fixed portion.
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