|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||G01C-023/00 G05D-001/00 G05D-003/00 G06F-007/00 G06F-017/00 B64C-039/00 B64C-017/02 B64C-021/00 B64C-023/00 B64C-023/08 F42B-010/62 F42B-010/02|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 1091|
A method for controlling a flying projectile which rotates during flight, comprising: determining an angle of rotation of an inertial mass spinning about an axis during flight; and controlling at least one actuator for altering at least a portion of an aerodynamic structure, selectively in dependence on the determined angle of rotation and a control input, to control aerodynamic forces during flight. An aerodynamic surface may rotate and interact with surrounding air during flight, to produce aerodynamic forces. A sensor determines an angular rotation of...
1. A flying projectile, comprising: an inertial mass, configured to spin during flight, about an axis of rotation to gyroscopically stabilize the flying projectile;an aerodynamic surface having a circular periphery, configured to interact and generate lift from forward movement of the flying projectile with respect to surrounding air during flight, to produce aerodynamic forces having an aerodynamic force profile having a center of pressure;a control system, configured to produce at least one control signal varying selectively in dependence on at least a...