Finite‐time attitude stabilization for rigid spacecraft
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Publication:5174437
DOI10.1002/rnc.3071zbMath1305.93178OpenAlexW1777141753MaRDI QIDQ5174437
Publication date: 17 February 2015
Published in: International Journal of Robust and Nonlinear Control (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1002/rnc.3071
Adaptive control/observation systems (93C40) Variable mass, rockets (70P05) Adaptive or robust stabilization (93D21) Variable structure systems (93B12)
Related Items (18)
Finite-time passivity of dynamic systems ⋮ Distributed adaptive containment control for second-order multi-agent systems via NTSM ⋮ Spacecraft Anti‐Unwinding Attitude Control Using Second‐Order Sliding Mode ⋮ Distributed attitude control for multiple flexible spacecraft under actuator failures and saturation ⋮ Nonlinear disturbance observer-based robust control of attitude tracking of rigid spacecraft ⋮ Super-twisting observer-based sliding mode control with fuzzy variable gains and its applications to fully-actuated hexarotors ⋮ Event‐triggered anti‐disturbance attitude control for rigid spacecrafts with multiple disturbances ⋮ Finite‐time attitude tracking control and vibration suppression for flexible spacecraft ⋮ Robust fixed-time attitude stabilization control of flexible spacecraft with actuator uncertainty ⋮ Finite-time attitude maneuvering and vibration suppression of flexible spacecraft ⋮ Adaptive finite-time command filtered fault-tolerant control for uncertain spacecraft with prescribed performance ⋮ Decentralized adaptive attitude synchronization control for spacecraft formation using nonsingular fast terminal sliding mode ⋮ Finite-time sliding mode attitude control for rigid spacecraft without angular velocity measurement ⋮ Continuous Fixed‐Time Controller Design for Dynamic Systems with Unmeasurable States Subject to Unbounded Disturbances ⋮ Continuous Fixed‐Time Convergent Super‐Twisting Algorithm in Case of Unknown State and Disturbance Initial Conditions ⋮ Adaptive finite-time attitude stabilization for rigid spacecraft with actuator faults and saturation constraints ⋮ Adaptive finite‐time actuator fault‐tolerant coordinated attitude control of multispacecraft with input saturation ⋮ Event-triggered backstepping control for attitude stabilization of spacecraft
Cites Work
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