Stabilisation of a flexible spacecraft subject to external disturbance and uncertainties
From MaRDI portal
Publication:2205304
DOI10.1155/2020/2906546zbMath1445.93014OpenAlexW3044917296MaRDI QIDQ2205304
Yun Fu, Lingxi Peng, Lingyan Hu, Yu Liu
Publication date: 20 October 2020
Published in: Complexity (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1155/2020/2906546
Control, switches and devices (``smart materials) in solid mechanics (74M05) Control/observation systems governed by partial differential equations (93C20) Adaptive control/observation systems (93C40) Vibrations in dynamical problems in solid mechanics (74H45)
Cites Work
- Unnamed Item
- Modeling and vibration control of a flexible aerial refueling hose with variable lengths and input constraint
- Semigroups of linear operators and applications to partial differential equations
- Active control of flexible systems
- Single parameter adaptive control of unknown nonlinear systems with tracking error constraints
- Composite learning sliding mode control of flexible-link manipulator
- Robust adaptive fault tolerant control for a linear cascaded ODE-beam system
- Positiveness and observer-based finite-time control for a class of Markov jump systems with some complex environment parameters
- Lyapunov approach to output feedback stabilization for the Euler-Bernoulli beam equation with boundary input disturbance
- Boundary cooperative control by flexible Timoshenko arms
- Vibration Control Of Flexible Spacecraft Integrating A Momentum Exchange Controller And A Distributed Piezoelectric Actuator
- Adaptive and optimal synchronization control of networked positive real infinite dimensional systems with virtual leader
- Grid Evolution Method for DOA Estimation
- Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver
- Boundary control of an axially moving accelerated/decelerated belt system
- Load reduction of a monopile wind turbine tower using optimal tuned mass dampers
This page was built for publication: Stabilisation of a flexible spacecraft subject to external disturbance and uncertainties