The Orion Microsatellite Mission: A Testbed for Command, Control, and Communications for Formation Fleets
msra(2001)
摘要
The Orion microsatellite, under development at Stanford University, will fly along with two other Stanford satellites ("Emeralds") as part of a NASA-funded project. The primary objective is to demonstrate, for the first time, the use of carrier-phase differential GPS (CDGPS) for the relative sensing, navigation and coordinated control of satellites to form a virtual spacecraft bus. Launch of this mission has been tentatively scheduled for late 2001. Formation flying offers an exciting new approach to conducting space science missions. Instead of employing a single, large satellite, a fleet of similar, smaller spacecraft is coordinated to perform mission-related tasks. While formation flying architectures have a significant amount of operational flexibility, the internal system complexity increases with the number of satellites in the fleet. In addition, constraints on satellite resources play a particularly key role. This paper is a summary of work conducted at Stanford to investigate the influence of resource constraints on mission and current-task planning. By making efficient use of knowledge associated with mission goals and operations, optimal strategies can be used to increase fleet life-cycle performance. In addition to discussing this topic, the role of the Orion mission as a testbed for these concepts is included.
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关键词
life cycle
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