On-line inertia estimation for use in controlling an aerospace vehicle
作者： Qinghong W. Wang , Manu Sharma
DOI:
关键词:
摘要: A system for controlling an aerospace vehicle using on-line inertia estimation may include attitude sensor to measure of the vehicle. The also a processor on board An estimator operable generate estimate rate and determine angular position velocity measurement movement orientation without any rates rotation being required.
lens.org 参考文章(27)
Qinghong W. Wang, Michael F. Barsky, Wobble and nutation control, and spin stabilization for a spacecraft using momentum conserving devices ,(1997)
Rongsheng Li, Yeong-Wei Andy Wu, Stable and verifiable state estimation methods and systems with spacecraft applications ,(2000)
Oliver Juckenhoefel, Michael Surauer, Walter Fichter, Method and system for the autonomous on-board determination of the position of a satellite ,(1998)
Toshiaki Yamashita, Maneuver device for artificial satellite ,(2002)
Michele Philippe Janvier, Anthony Philip Astrium Limited Holt, Autonomous manoeuvring for spinning spacecraft ,(2002)
Loren I. Slafer, Sibnath Basuthakur, On-board three-axes attitude determination and control system ,(1992)
Masaru Fukuda, Hiroyuki Toda, Attitude sensing apparatus for determining the attitude of a mobile unit ,(2004)
Dan Y. Liu, Qinghong W. Wang, Richard Y. Chiang, Systems and method of controlling a spacecraft using attitude sensors ,(2008)
Jason A Keim, A Behcet Acikmese, Joel F Shields, None, Spacecraft inertia estimation via constrained least squares ieee aerospace conference. pp. 1655995- ,(2006) , 10.1109/AERO.2006.1655995
Richard Y. Chiang, Tung-Ching Tsao, Gyroless transfer orbit sun acquisition using only wing current measurement feedback ,(2009)