发明名称 Micro-satellite and satellite formation for inverse and distributed proximity operations
摘要 A method and apparatus for conducting proximity operations is disclosed. The method called inverser proximity operations includes maneuvering an active vehicle into general proximity to a target vehicle, transmitting from the target vehicle to the active vehicle data representing relative position and velocity between the target vehicle and the active vehicle, and maneuvering the active vehicle in accordance with the data to effect a desired proximity operation. Another method called distributed proximity operations includes maneuvering a carrier vehicle into general proximity to a target vehicle, releasing one or more active vehicles from the carrier vehicle, transmitting from the carrier vehicle to the active vehicle(s) data representing relative position and velocity between the target vehicle and the active vehicle, and maneuvering the active vehicle(s) in accordance with the data to effect a desired proximity operation. The proximity operations are similarly suitable for aeronautical systems, such as when using an active aircraft to re-fuel a target aircraft, such as a drone. Whether for space, air, or other environments, the proximity operations described can be used for re-fueling, repairing, and replacing components and/or systems.
申请公布号 US6845303(B1) 申请公布日期 2005.01.18
申请号 US20020287683 申请日期 2002.11.05
申请人 LOCKHEED MARTIN CORPORATION 发明人 BYLER ERIC ALAN
分类号 B64D39/00;B64G1/10;B64G1/40;B64G1/64;G05D1/12;(IPC1-7):B64C1/00;G05D1/00;G06F1/00;G06F17/10;G05G7/78 主分类号 B64D39/00
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