Keywords: کنترل نگرش فضاپیمای; Spacecraft attitude control; Redundant reaction wheels; Actuator failures; Nonlinear adaptive control; Multivariable systems;
مقالات ISI کنترل نگرش فضاپیمای (ترجمه نشده)
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Keywords: کنترل نگرش فضاپیمای; Spacecraft attitude control; Hybrid actuation; Switched systems; Switching time-optimal control; Numerical optimal control;
Keywords: کنترل نگرش فضاپیمای; Multi-objective optimization; Graceful performance degradation; Active fault tolerant control; Reference trajectory management; Spacecraft attitude control; Pareto optimal set;
Keywords: کنترل نگرش فضاپیمای; Earth's magnetic field models; Spacecraft attitude control; Linear and nonlinear transformation; Orbital frame; Body frame;
Keywords: کنترل نگرش فضاپیمای; Spacecraft attitude control; Robust control; Optimal control;
Keywords: کنترل نگرش فضاپیمای; Spacecraft formation flying; Spacecraft attitude control; Line-of-sight;
Keywords: کنترل نگرش فضاپیمای; Line-of-sight based control; Spacecraft attitude control; Spacecraft formation flying; Coordinate-free attitude control;
Keywords: کنترل نگرش فضاپیمای; Spacecraft attitude control; Neuro-fuzzy network; State-dependent Riccati equation; Approximated optimal feedback controller
Keywords: کنترل نگرش فضاپیمای; Spacecraft charging; Spacecraft attitude control; High voltage experimentation;
Keywords: کنترل نگرش فضاپیمای; Finite time; Fast terminal sliding mode control; Double closed loops; Spacecraft attitude control;
Keywords: کنترل نگرش فضاپیمای; Periodic Riccati equation; LQR; Spacecraft attitude control; Magnetic torque;
Keywords: کنترل نگرش فضاپیمای; Underactuated spacecraft; Spacecraft attitude control; Tube-based MPC; Fault tolerant control
An efficient LQR design for discrete-time linear periodic system based on a novel lifting method
Keywords: کنترل نگرش فضاپیمای; Linear periodic discrete-time system; Periodic algebraic Riccati equation; LQR; Spacecraft attitude control; Magnetic torque;
A Perturbed Chord (Newton-Kantorovich) Method for Constrained Nonlinear Model Predictive Control
Keywords: کنترل نگرش فضاپیمای; Model Predictive Control; Nonlinear Systems; Constrained Control; Numerical Optimization Algorithms; Newton-Kantorovich Method; Spacecraft Attitude Control; Engine Control; Powertrain Control;
Research ArticleRobust fault-tolerant tracking control design for spacecraft under control input saturation
Keywords: کنترل نگرش فضاپیمای; Spacecraft attitude control; Robust fault tolerant; Multiplicative actuator fault;
Inverse optimal and robust nonlinear attitude control of rigid spacecraft
Keywords: کنترل نگرش فضاپیمای; Inverse optimal control; Robust control; Spacecraft attitude control
Attitude and orbit control systems for the LISA Pathfinder mission
Keywords: کنترل نگرش فضاپیمای; AOCS; Spacecraft attitude control; DFACS; Spacecraft GNC; FEEP
Spacecraft attitude control via a combined state-dependent Riccati equation and adaptive neuro-fuzzy approach
Keywords: کنترل نگرش فضاپیمای; Spacecraft attitude control; State-dependent Riccati equation; Adaptive neuro-fuzzy approach
Two degree-of-freedom spacecraft attitude controller
Keywords: کنترل نگرش فضاپیمای; Spacecraft attitude control; PD controller; AFC technique
Sustainer electric propulsion system application for spacecraft attitude control
Keywords: کنترل نگرش فضاپیمای; Electric propulsion; Spacecraft attitude control;
Adaptive attitude control of spacecraft without velocity measurements using Chebyshev neural network
Keywords: کنترل نگرش فضاپیمای; Spacecraft attitude control; Adaptive control; Neural network
Adaptive attitude control of spacecraft using neural networks
Keywords: کنترل نگرش فضاپیمای; Adaptive control; Neural networks; Spacecraft attitude control
Research on optimal guaranteed cost control of flexible spacecraft*
Keywords: کنترل نگرش فضاپیمای; spacecraft attitude control; Euler-Bernoulli beam; optimal guaranteed cost control;
Robust and optimal attitude stabilization of spacecraft with external disturbances
Keywords: کنترل نگرش فضاپیمای; Spacecraft attitude control; Robust control; Optimal control; Minimax approach;
A new steering law for redundant control moment gyroscope clusters
Keywords: کنترل نگرش فضاپیمای; Control moment gyroscopes; Steering law; Inverse kinematics algorithm; Spacecraft attitude control;
Flexible spacecraft attitude maneuver by application of sliding mode control
Keywords: کنترل نگرش فضاپیمای; Spacecraft attitude control; Sliding mode control; Boundary torque; Output feedback; Flexible spacecraft;