2004
DOI: 10.1109/tac.2003.821406
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A Simple Velocity-Free Controller for Attitude Regulation of a Spacecraft With Delayed Feedback

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Cited by 46 publications
(47 citation statements)
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“…Unfortunately, very few literatures set foot in the output feedback control for disturbed nonlinear systems with input delay compensation. In Alion et al, 30 output feedback controllers were proposed to stabilize nonlinear systems with constant input delay by using the linearization method, which will cause some deviations from the realistic systems and may result in instability of the closed-loop system. Observer-based output feedback control were synthesized in Zha et al 31 and Jo et al 32 for a class of feedforward nonlinear systems with time-varying delay in the control input.…”
Section: Introductionmentioning
confidence: 99%
“…Unfortunately, very few literatures set foot in the output feedback control for disturbed nonlinear systems with input delay compensation. In Alion et al, 30 output feedback controllers were proposed to stabilize nonlinear systems with constant input delay by using the linearization method, which will cause some deviations from the realistic systems and may result in instability of the closed-loop system. Observer-based output feedback control were synthesized in Zha et al 31 and Jo et al 32 for a class of feedforward nonlinear systems with time-varying delay in the control input.…”
Section: Introductionmentioning
confidence: 99%
“…In [43] and [44], a backstepping approach that utilizes ODE-PDE cascade transformation for input delayed systems is extended to nonlinear control systems with an actuator delay of unrestricted length. The results in [45]- [47] utilize controllers developed for delay-free systems and prove robustness to the delay provided certain delay dependent conditions hold true. Also, these results only establish local exponential or asymptotic stability for a zero/stationary solution of uncertain nonlinear systems (linearized about a setpoint).…”
mentioning
confidence: 97%
“…For example, in [1], the problem was addressed assuming known, constant and sufficiently small delays, using modified Rodrigues parameters to represent attitude. In [3], rotation matrices were used to describe attitude, and delays were also considered constant and known.…”
Section: Introductionmentioning
confidence: 99%
“…Using quaternion representation, [16] considered both attitude and angular velocity subjected to constant delays; stability conditions rely only on initial velocities and delay magnitude. In [17], angular velocity measurements are discarded, and stability conditions are derived with only attitude measurements, as in [1]. Sufficient conditions that simultaneously guarantee stability and H ∞ performance were given in [23], which also addressed time-varying delays.…”
Section: Introductionmentioning
confidence: 99%