Minimum-Time Reorientation of Axisymmetric Rigid Spacecraft Using Three Controls-Reference-Cited by-同舟云学术

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Minimum-Time Reorientation of Axisymmetric Rigid Spacecraft Using Three Controls

Published:2022-11 Issue:6 Volume:59 Page:2195-2201
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Pager Elisha R.¹^ORCID,Rao Anil V.¹^ORCID

Affiliation:

1. University of Florida, Gainesville, Florida 32611

Funder

Air Force Research Laboratory

Office of Naval Research

US National Science Foundation Division of Civil, Mechanical and Manufacturing Innovation

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A35422

Reference16 articles.

1. Time-optimal three-axis reorientation of a rigid spacecraft

2. Time-Optimal Control of Axisymmetric Rigid Spacecraft Using Two Controls

3. Optimal Control of Spinning Axisymmetric Spacecraft: A Pseudospectral Approach

4. Singular Control in Minimum Time Spacecraft Reorientation

Cited by 3 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. A Unified Trajectory Generation Algorithm for Dynamic Dexterous Manipulation;2023 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS);2023-10-01

2. Spacecraft Coupled Roto-translational Time-Optimal Control for Rendezvous Missions;The Journal of the Astronautical Sciences;2023-07-13

3. L2 Norm-Based Control Regularization for Solving Optimal Control Problems;IEEE Access;2023

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