TY - JOUR
T1 - Adaptive tracking control using synthesized velocity from attitude measurements
AU - Wong, H.
AU - de Queiroz, M. S.
AU - Kapila, V.
N1 - Funding Information:
This paper was not presented at any IFAC meeting. This paper was recommended for publication in revised form by Associate Editor B. Brogliato under the direction of Editor Frank Lewis. This work was supported in part by the Air Force Office of Scientific Research under grant F49620-93-C-0063, the Air Force Research Lab/VAAD, WPAFB, OH, under IPA: Visiting Faculty Grant, and the NASA/New York Space Grant Consortium under grant 32310-5891.
Copyright:
Copyright 2004 Elsevier Science B.V., Amsterdam. All rights reserved.
PY - 2000
Y1 - 2000
N2 - The attitude tracking problem of uncertain rigid spacecraft without angular velocity measurements is addressed in this paper. The adaptive control law, which incorporates a velocity-generating filter from attitude measurements, is shown to ensure the asymptotic convergence of the attitude and angular velocity tracking errors despite unknown spacecraft inertia. Simulation results are presented to illustrate the theoretical results.
AB - The attitude tracking problem of uncertain rigid spacecraft without angular velocity measurements is addressed in this paper. The adaptive control law, which incorporates a velocity-generating filter from attitude measurements, is shown to ensure the asymptotic convergence of the attitude and angular velocity tracking errors despite unknown spacecraft inertia. Simulation results are presented to illustrate the theoretical results.
UR - http://www.scopus.com/inward/record.url?scp=0034548551&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0034548551&partnerID=8YFLogxK
M3 - Conference article
AN - SCOPUS:0034548551
SN - 0743-1619
VL - 3
SP - 1572
EP - 1576
JO - Proceedings of the American Control Conference
JF - Proceedings of the American Control Conference
T2 - 2000 American Control Conference
Y2 - 28 June 2000 through 30 June 2000
ER -