On the attitude stabilization of a rigid spacecraft using two skew control moment gyros
From MaRDI portal
Publication:494779
DOI10.1007/S11071-014-1796-0zbMath1318.70024OpenAlexW2037420344MaRDI QIDQ494779
Jun Zhang, Lei Jin, Shi-Jie Xu, Hai-Chao Gui
Publication date: 2 September 2015
Published in: Nonlinear Dynamics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s11071-014-1796-0
Variable mass, rockets (70P05) Adaptive or robust stabilization (93D21) Control of mechanical systems (70Q05) Variable structure systems (93B12) Synthesis problems (93B50)
Related Items (5)
Chaotic attitude analysis of a satellite via Lyapunov exponents and its robust nonlinear control subject to disturbances and uncertainties ⋮ Dual-quaternion-based adaptive motion tracking of spacecraft with reduced control effort ⋮ Adaptive integral sliding mode control for spacecraft attitude tracking with actuator uncertainty ⋮ Agile attitude maneuver with active vibration-suppression for flexible spacecraft ⋮ Robust control for uncertain impulsive systems with input constraints and external disturbance
Cites Work
- Unnamed Item
- Unnamed Item
- Unnamed Item
- Fault-tolerant sliding mode attitude control for flexible spacecraft under loss of actuator effectiveness
- On the attitude stabilization of rigid spacecraft
- Singularly perturbed feedback linearization with linear attitude deviation dynamics realization
- Global asymptotic stabilization of the attitude and the angular rates of an underactuated non-symmetric rigid body
- Comments on the stabilizability of the angular velocity of a rigid body
- Subanalytic sets and feedback control
- Second-order conditions for local controllability
- Attitude stabilization of a rigid spacecraft using two control torques: A nonlinear control approach based on the spacecraft attitude dynamics
- Control of underactuated spacecraft with bounded inputs
- A novel approach to the attitude control of axisymmetric spacecraft
- Robust fault-tolerant control for flexible spacecraft against partial actuator failures
- Global feedback stabilization of the angular velocity of a symmetric rigid body
- Underactuated spacecraft angular velocity stabilization and three-axis attitude stabilization using two single gimbal control moment gyros
- Inverse dynamics of servo-constraints based on the generalized inverse
- Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body models
- Spin-axis stabilisation of underactuated rigid spacecraft under sinusoidal disturbance
- Asymptotic perturbed feedback linearisation of underactuated Euler's dynamics
- Time-varying exponential stabilization of a rigid spacecraft with two control torques
- Attitude stabilization of a rigid spacecraft using two momentum wheel actuators
- Controllability of Spacecraft Attitude Using Control Moment Gyroscopes
- Spin-axis stabilization of symmetric spacecraft with two control torques
This page was built for publication: On the attitude stabilization of a rigid spacecraft using two skew control moment gyros
