Attitude takeover control of spacecraft based on neural network predefined-time extended state observer
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Publication:6591212
DOI10.1002/RNC.7493zbMATH Open1545.93173MaRDI QIDQ6591212
Mingyue Shi, Baolin Wu, Franco Bernelli-Zazzera
Publication date: 21 August 2024
Published in: International Journal of Robust and Nonlinear Control (Search for Journal in Brave)
neural networkactuator installation deviationattitude takeover controlpredefined-time observerunmeasurable angular velocity
Cites Work
- Attitude control of rigid spacecraft with predefined-time stability
- Prescribed-time output feedback for linear systems in controllable canonical form
- Sliding mode control using modified Rodrigues parameters
- A class of predefined-time stable dynamical systems
- A novel sth‐order observer for linear system: Application to state and fault estimation of spacecraft control system
- A coupled nonlinear spacecraft attitude controller and observer with an unknown constant gyro bias and gyro noise
- Nonlinear Feedback Design for Fixed-Time Stabilization of Linear Control Systems
- Anti‐unwinding adaptive spacecraft attitude tracking control based on similar skew‐symmetric structures
- Constrained <scp>multi‐observer‐based fault‐tolerant disturbance‐rejection</scp> control for rigid spacecraft
- Predefined-time formation control of the quadrotor-UAV cluster' position system
- Fault-tolerant control for full-state error constrained attitude tracking of uncertain spacecraft
- An adaptive time‐varying barrier Lyapunov function‐based attitude tracking control for spacecrafts without angular velocity measurement
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