Optimization of Spacecraft Thruster Management Function-Reference-Cited by-同舟云学术

Optimization of Spacecraft Thruster Management Function

Published:2005-11 Issue:6 Volume:28 Page:1283-1290
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Ankersen Finn,Wu Shu-Fan,Aleshin Alexander,Vankov Alexander,Volochinov Vladimir

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.11531

Reference15 articles.

1. An Advanced Spacecraft Autopilot Concept

2. Configuration design and efficient operation of redundant multi-jet systems

3. 3Paradiso, J. A. "A Highly Adaptable Steering/Selection Procedure for Combined CMG/RCS Spacecraft Control, Detailed Report," C. S. Draper Lab., Report CSDL-R-1835, Cambridge, MA, March 1986.

4. 4Paradiso, J. A. "Application of Linear Programming to Coordinated Management of Jets and Aerosurfaces for Aerospace Vehicle Control," C. S. Draper Lab., Report CSDL-R-2065, Cambridge, MA, Nov. 1988.

5. Adaptable method of managing jets and aerosurfaces for aerospace vehicle control

Cited by 12 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Convex MPC and Thrust Allocation With Deadband for Spacecraft Rendezvous;IEEE Control Systems Letters;2024

2. An Integral-based Control Allocation Algorithm for Optimal Spacecraft Actuator Selection under l₁, l₂, l_∞ Criteria for Fault Tolerance;2023 31st Mediterranean Conference on Control and Automation (MED);2023-06-26

3. Distributed optimal control allocation for 6-dof spacecraft with redundant thrusters;Aerospace Science and Technology;2021-11

4. Satellite Thrusters’ Control Allocation and Application Used for Integrated Attitude-Orbit Control System;Lecture Notes in Electrical Engineering;2021

5. Efficient Thrust Management Algorithm for Variable Thrust Solid Propulsion System with Multi-Nozzles;Journal of Spacecraft and Rockets;2020-03