Fixed‐time attitude tracking control for spacecraft based on adding power integrator technique

DOI10.1002/rnc.4897zbMath1465.93105OpenAlexW3006150162MaRDI QIDQ4990452

Shixi Hou, Boyan Jiang, Guangfu Ma, Chuanjiang Li

Publication date: 28 May 2021

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.4897

zbMATH Keywords

adaptive controlfinite-time controladding a power integratorfixed-time controlspacecraft attitude tracking

Mathematics Subject Classification ID

Application models in control theory (93C95) Adaptive control/observation systems (93C40) Finite-time stability (93D40)

Related Items (10)

Predefined‐time control of cooperative manipulators ⋮ Output feedback stabilization within prescribed finite time of asymmetric time‐varying constrained nonholonomic systems ⋮ Constrained fast finite‐time exact tracking for disturbed nonlinear systems ⋮ Guaranteed cost control of rigid‐body attitude systems under control saturation ⋮ Predefined‐time tracking control for high‐order nonlinear systems with control saturation ⋮ Barrier Lypunov functions‐based nonsingular fixed‐time switching control for strict‐feedback nonlinear dynamics with full state constraints ⋮ Continuous precise predefined-time attitude tracking control for a rigid spacecraft ⋮ Continuous appointed‐time prescribed performance attitude tracking control for rigid spacecraft with actuator faults on SO(3) ⋮ Event-triggered adaptive fixed-time fuzzy control for uncertain nonlinear systems with unknown actuator faults ⋮ Neural learning fixed-time adaptive tracking control of complex stochastic constraint nonlinear systems

This page was built for publication: Fixed‐time attitude tracking control for spacecraft based on adding power integrator technique