发明名称 |
SYSTEM AND METHOD FOR ATTITUDE CONTROL OF A FLIGHT VEHICLE USING PITCH-OVER THRUSTERS |
摘要 |
A reliable and inexpensive attitude control system uses a plurality of pitch-over thrusters to perform rapid and precise attitude maneuvers for a flight vehicle. The pitch-over thrusters create rotational moments that directly pitch and yaw the flight vehicle. The use of very simple thrusters and control techniques provides for a reliable and cost effective solution. The ability to perform overlapping pitch and yaw maneuvers with single-shot fixed-impulse thrusters provides for high-speed maneuverability.
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申请公布号 |
US2009072076(A1) |
申请公布日期 |
2009.03.19 |
申请号 |
US20060470900 |
申请日期 |
2006.09.07 |
申请人 |
RAYTHEON COMPANY |
发明人 |
BRINKERHOFF ROBERT;MAHNKEN MICHAEL;LOEHR RICHARD;COOK JAMES |
分类号 |
F42B15/01 |
主分类号 |
F42B15/01 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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