A Closed-Loop Hardware Simulation of Decentralized Satellite Formation Control
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Summary
Hardware experimentation has been extended to include closed-loop integrated guidance and navigation of multiple spacecraft formations using GPS receivers and real-time vehicle telemetry.
- Type
- article
- Published
- 2002-01-01
- Cited by
- 2
- References
- 9
- OpenAlex
- https://openalex.org/W168824637
- Semantic Scholar
- https://api.semanticscholar.org/CorpusID:107707419
Keywords
Global Positioning System, Linear-quadratic-Gaussian control, Satellite, Kalman filter, Computer science
References
- TechSat 21: formation design, control, and simulation
- Sensing technologies for formation-flying spacecraft in LEO using CDGPS and an interspacecraft communications system
- Enabling Spacecraft Formation Flying through Spaceborne GPS and Enhanced Automation Technologies
- Understanding GPS : principles and applications
- Hot Start of GPS Receivers for LEO Microsatellites
- A GPS Receiver for Space Applications
- Ground Experimentation of a Pseudolite-Only Method for the Relative Positioning of Two Spacecraft
- Computation and transmission requirements for a decentralized linear-quadratic-Gaussian control problem
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