Optimal Finite Thrust Rendezvous Maneuvers of Chaser Spacecraft Towards Capturing Target Object-Reference-Cited by-同舟云学术

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Optimal Finite Thrust Rendezvous Maneuvers of Chaser Spacecraft Towards Capturing Target Object

Published:2024-01-04 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2024 Forum
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Author:

Sah Roshan¹,Srivastava Raunak¹,Saha Somdeb¹,Das Kaushik¹

Affiliation:

1. Tata Consultancy Services Ltd

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2024-1633

Reference26 articles.

1. Design Development of Debris Chaser Small Satellite with Robotic Manipulators for Debris Removal

2. Attitude Determination and Control System for a LEO Debris Chaser Small Satellite

3. Free Floating and Rotation Floating approaches for Control of Space Robots: A comparative study

Cited by 2 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. Target Grasp-conditioned Whole-body Control of Satellite Manipulators using Neural Fields with MPC;2024 IEEE Aerospace Conference;2024-03-02

2. Numerical Modeling of Liquid Propellant Mass Transfer with Sloshing during On-Orbit Refueling;2024 IEEE Aerospace Conference;2024-03-02

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