TY - GEN
T1 - Observer-based delayed feedback attitude control for single- and multi-actuator maneuvers
AU - Torkamani, Shahab
AU - Nazari, Morad
AU - Samiei, Ehsan
AU - Butcher, Eric A.
PY - 2013
Y1 - 2013
N2 - Observer-based attitude controllers for single- and multi-actuator maneuvers are developed from the delayed state feedback control laws obtained by the Lyapunov-Krasovskii functional and inverse dynamics approaches, respectively. The TRIAD algorithm is employed to process the observations. The observer gain is selected based on the extended Kalman-Bucy (EKB) filter, and a novel delay estimation approach is used to provide the estimates of the delay. The observer-based delayed feedback control laws are shown to be capable of accurate control of spacecraft attitude from noise-corrupted attitude measurements.
AB - Observer-based attitude controllers for single- and multi-actuator maneuvers are developed from the delayed state feedback control laws obtained by the Lyapunov-Krasovskii functional and inverse dynamics approaches, respectively. The TRIAD algorithm is employed to process the observations. The observer gain is selected based on the extended Kalman-Bucy (EKB) filter, and a novel delay estimation approach is used to provide the estimates of the delay. The observer-based delayed feedback control laws are shown to be capable of accurate control of spacecraft attitude from noise-corrupted attitude measurements.
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U2 - 10.1109/acc.2013.6579961
DO - 10.1109/acc.2013.6579961
M3 - Conference contribution
AN - SCOPUS:84883507802
SN - 9781479901777
T3 - Proceedings of the American Control Conference
SP - 964
EP - 969
BT - 2013 American Control Conference, ACC 2013
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2013 1st American Control Conference, ACC 2013
Y2 - 17 June 2013 through 19 June 2013
ER -