发明名称 |
EMPLOYING BOOSTER TRAJECTORY IN A PAYLOAD INERTIAL MEASUREMENT UNIT |
摘要 |
A payload launching method measures the attitude of a booster during a launch with an inertial measurement unit on the payload to compare the actual booster trajectory with a desired trajectory to control the payload at the deployment location, the inertial measurement unit on a booster carrying the payload using said desired trajectory to reach the deployment location |
申请公布号 |
EP1311428(B1) |
申请公布日期 |
2010.10.27 |
申请号 |
EP20010964389 |
申请日期 |
2001.08.23 |
申请人 |
HONEYWELL INTERNATIONAL INC. |
发明人 |
KAU, SHING, PETER |
分类号 |
B64G1/24;B64G1/00;B64G1/28;F41G7/36;G01C21/16;G05D1/08;G05D1/10 |
主分类号 |
B64G1/24 |
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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