Sliding mode control using modified Rodrigues parameters
From MaRDI portal
Publication:3126910
DOI10.2514/3.21798zbMath0865.93044OpenAlexW2123411533MaRDI QIDQ3126910
F. Landis Markley, John L. Crassidis
Publication date: 29 May 1997
Published in: Journal of Guidance, Control, and Dynamics (Search for Journal in Brave)
Full work available at URL: https://semanticscholar.org/paper/b5858ce3c065688c4813496048cad45429841e63
Related Items (21)
Robust adaptive sliding mode attitude maneuvering and vibration damping of three-axis-stabilized flexible spacecraft with actuator saturation limits ⋮ Sliding mode maneuvering control and active vibration damping of three-axis stabilized flexible spacecraft with actuator dynamics ⋮ Fault reconstruction approach for distributed coordinated spacecraft attitude control system ⋮ Chaotic attitude control of satellite using impulsive control ⋮ Anti-unwinding sliding mode attitude control via two modified Rodrigues parameter sets for spacecraft ⋮ Robust non-aggressive three-axis attitude control of spacecraft: dynamic sliding mode approach ⋮ Singularity avoidance controller design for spacecraft attitude control using double-gimbal variable-speed control moment gyro ⋮ Filtering‐based concurrent learning adaptive attitude tracking control of rigid spacecraft with inertia parameter identification ⋮ An anti-disturbance PD control scheme for attitude control and stabilization of flexible spacecrafts ⋮ Consensus on SO(3) with piecewise-continuous sinusoids ⋮ Nonlinear disturbance observer based adaptive super-twisting sliding mode control for generic hypersonic vehicles with coupled multisource disturbances ⋮ Adaptive finite-time command filtered fault-tolerant control for uncertain spacecraft with prescribed performance ⋮ Finite-time control for attitude tracking maneuver of rigid satellite ⋮ Integrated nonlinear optimal control of spacecraft in proximity operations ⋮ Orientation control on SO(3) with piecewise sinusoids ⋮ Neural network-based adaptive attitude tracking control for flexible spacecraft with unknown high-frequency gain ⋮ Control of Three-axis Stabilized Flexible Spacecraft Using Variable Structure Strategies Subject to Input Nonlinearities ⋮ Adaptive Variable Structure and Active Vibration Reduction for Flexible Spacecraft under Input Nonlinearity ⋮ Adaptive variable structure maneuvering control and vibration reduction of three-axis stabilized flexible spacecraft ⋮ Finite-time fuzzy game-based attitude control for on-orbit cooperative transporting ⋮ Attitude Control for Rigid Satellite Under Actuator Constraint
This page was built for publication: Sliding mode control using modified Rodrigues parameters
