As for the problem of precise guidance in the process of remote autonomous orbit maneuver, a guidance strategy allowing various guidance law diverse combinations in different stage is presented. Comparing with the existing method, the advantages of various guidance laws has been combined in this new strategy. It not only saves fuel and easy to be engineering, but also notably improves the precision of guidance, and makes spacecraft has the capability of autonomous orbit maneuver to remote target orbit accurately.
Research on the precision combined guidance technology of remote autonomous orbital maneuver
2013-07-01
248390 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Combined aerodynamic-propulsive orbital plane change maneuver
Engineering Index Backfile | 1965
|Suboptimal Guidance for Orbital Proximity Maneuver with Path Constraints Capability
British Library Conference Proceedings | 2012
|