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.
申请公布号
WO2008048702(A3)
申请公布日期
2008.10.02
申请号
WO2007US63398
申请日期
2007.03.06
申请人
RAYTHEON COMPANY;BRINKERHOFF, ROBERT;MAHNKEN, MICHAEL;LOEHR, RICHARD;COOK, JAMES;CAVALLERI, ROBERT
发明人
BRINKERHOFF, ROBERT;MAHNKEN, MICHAEL;LOEHR, RICHARD;COOK, JAMES;CAVALLERI, ROBERT