Discrete gain scheduling control approach to elliptical orbit rendezvous system with actuator saturation
DOI10.1002/rnc.6509OpenAlexW4310988702MaRDI QIDQ6149795
Jianqiao Wang, Unnamed Author, Kok Lay Teo, Xiang-Yu Gao, Hongfu Yang
Publication date: 6 February 2024
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.6509
invariant setactuator saturationperiodic Riccati equationspacecraft rendezvousdiscrete gain scheduling control
Feedback control (93B52) Linear systems in control theory (93C05) Orbital mechanics (70M20) Control/observation systems governed by ordinary differential equations (93C15)
Cites Work
- Unnamed Item
- Unnamed Item
- Two new modified Gauss-Seidel methods for linear system with M-matrices
- On semi-global stabilization of linear periodic systems with control magnitude and energy saturations
- Set invariance in control
- Output feedback gain scheduled control of actuator saturated linear systems with applications to the spacecraft rendezvous
- Stability analysis and control synthesis for linear systems with non-symmetrical input saturation
- Output feedback robust \(H_\infty\) control for spacecraft rendezvous system subject to input saturation: A gain scheduled approach
- Shorter Notes: The Roots of a Polynomial Vary Continuously as a Function of the Coefficients
- State Transition Matrices for Terminal Rendezvous Studies: Brief Survey and New Example
- Cauchy's Interlace Theorem for Eigenvalues of Hermitian Matrices
- Robust control for spacecraft rendezvous system with actuator unsymmetrical saturation: a gain scheduling approach
- An optimal control approach to spacecraft rendezvous on elliptical orbit
- Robust H∞ dynamic output feedback control for spacecraft rendezvous with poles and input constraint
- Non-fragile robustH∞control for uncertain spacecraft rendezvous system with pole and input constraints
- Control systems with actuator saturation: analysis and design
- Parametric Lyapunov equation based event‐triggered and self‐triggered control of input constrained linear systems
- Event‐triggered and self‐triggered gain scheduling control of input constrained systems with applications to the spacecraft rendezvous
This page was built for publication: Discrete gain scheduling control approach to elliptical orbit rendezvous system with actuator saturation