Velocity-to-Be-Gained Deorbit Guidance Law Using State Space Perturbation Method-Reference-Cited by-同舟云学术

Velocity-to-Be-Gained Deorbit Guidance Law Using State Space Perturbation Method

Published:2018-03 Issue:2 Volume:31 Page:04017099
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhang Hongbo¹,Li Bin²

Affiliation:

1. Associate Professor, College of Aerospace Science and Engineering, National Univ. of Defense Technology, No. 109, Deya Rd., Kaifu District, Changsha, Hunan 410073, China (corresponding author).

2. Doctoral Student, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Deya Rd., Kaifu District, Changsha, Hunan 410073, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000808

Reference20 articles.

1. Dynamics of Large Debris Connected to Space Tug by a Tether

2. Baldwin M. C. (2010). “Autonomous optimal deorbit guidance.” Ph.D. dissertation Iowa State Univ. Ames IA.

3. Optimal Deorbit Guidance

4. Baldwin M. C. Pan B. and Lu P. (2009). “On autonomous optimal deorbit guidance.” AIAA Guidance Navigation and Control Conf. AIAA Reston VA.

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