发明名称 |
THRUST VECTORING A FLIGHT VEHICLE DURING HOMING USING A MULTI-PULSE MOTOR |
摘要 |
A method and apparatus for thrust vectoring a flight vehicle during homing are disclosed. The flight vehicle includes a body; a plurality of attitude control mechanisms on the body; a multi-pulse motor housed at least partially in the body; and a control unit housed in the body. The control unit generates signals controlling an actuation of the attitude control mechanisms and the multi-pulse motor to initiate a follow-on burn of the multi-pulse motor to effect a maneuver directed by the actuation of the attitude control mechanisms. The method includes conserving a second burn of a dual pulse motor until target acquisition; acquiring a target; actuating a attitude control mechanism for the flight vehicle to alter the flight vehicle's heading; and initiating the second burn. |
申请公布号 |
WO2004038208(A2) |
申请公布日期 |
2004.05.06 |
申请号 |
WO2003US09656 |
申请日期 |
2003.03.31 |
申请人 |
LOCKHEED MARTIN CORPORATION |
发明人 |
BROWN, CHARLES, C.;BEYER, PHILIP, T. |
分类号 |
F02K9/28;F02K9/42;F02K9/80;F02K9/94;F42B10/64;F42B10/66;F42B15/01 |
主分类号 |
F02K9/28 |
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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