Position and attitude control of a spacecraft using the state-dependent Riccati equation technique-Reference-Cited by-同舟云学术

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Position and attitude control of a spacecraft using the state-dependent Riccati equation technique

Published:2000 Issue: Volume: Page:
ISSN:
Container-title:Proceedings of the 2000 American Control Conference. ACC (IEEE Cat. No.00CH36334)
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Author:

Stansbery D.T.,Cloutier J.R.

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx5/7046/19019/00879525.pdf?arnumber=879525

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