Design and Control of Approach Trajectory by Impulsive Velocity Change-Reference-Cited by-同舟云学术

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Design and Control of Approach Trajectory by Impulsive Velocity Change

Published:2004 Issue:611 Volume:52 Page:572-578
ISSN:1344-6460
Container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:ja
Short-container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

Sugahara Masayuki,Masutani Yasuhiro,Miyazaki Fumio

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass/52/611/52_611_572/_pdf

Reference8 articles.

1. Space robot. Interview to Mr. Koichi Wakata, a Japanese Mission Specialist of the Space Shuttle.

2. Potential-Function Guidance Forming Eccentricity Separation of Satellites with Continuous Thrust.

3. Optimal impulsive space trajectories based on linear equations

4. Quadratic-Based Computation of Four-Impulse Optimal Rendezvous near Circular Orbit

Cited by 1 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. Initiative of Zero Debris Collision Area with Impulsive Rendezvous;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2011

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