On spacecraft maneuvers control subject to propellant engine modes
Author:
Funder
Islamic Azad University
Publisher
Elsevier BV
Subject
Applied Mathematics,Control and Systems Engineering,Electrical and Electronic Engineering,Computer Science Applications,Instrumentation
Reference40 articles.
1. Autonomous distributed control of simultaneous multiple spacecraft proximity maneuvers;McCamish;IEEE Trans Autom Sci Eng,2010
2. Quasi-continuous higher order sliding-mode controllers for spacecraft-attitude-tracking maneuvers;Pukdeboon;IEEE Trans Ind Electron,2010
3. Flight-like ground demonstrations of precision maneuvers for spacecraft formations—Part I;Scharf;IEEE Syst J,2010
4. Flight-like ground demonstrations of precision maneuvers for spacecraft formations—Part II;Scharf;IEEE Syst J,2010
5. Navigation solution to maneuver a spacecraft relative to multiple satellites and ground locations;Leigh;Acta Astronaut,2015
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2. Design of a robust fault-tolerant control algorithm based on failure mode effects criticality analysis for a three-axis satellite;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2017-08-31
3. Application of hybrid robust three-axis attitude control approach to overactuated spacecraft—A quaternion based model;Journal of Central South University;2016-07
4. Stability analysis of autonomous space systems in the presence of large disturbances: A Lyapunov-based constrained control strategy;ISA Transactions;2016-03
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