Minimizing the Effects of Impulsive Orbit Maneuver Uncertainty-Reference-Cited by-同舟云学术

Minimizing the Effects of Impulsive Orbit Maneuver Uncertainty

Published:2018-09 Issue:5 Volume:31 Page:04018055
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhang Gang¹,Geng Yunhai²

Affiliation:

1. Associate Professor, Research Center of Satellite Technology, Harbin Institute of Technology, 150001 Heilongjiang, People’s Republic of China (corresponding author).

2. Professor, Research Center of Satellite Technology, Harbin Institute of Technology, 150001 Heilongjiang, People’s Republic of 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.1943-5525.0000890

Reference18 articles.

1. An Introduction to the Mathematics and Methods of Astrodynamics, Revised Edition

2. Linear Covariance Techniques for Orbital Rendezvous Analysis and Autonomous Onboard Mission Planning

3. Initial Relative Orbit Determination Analytical Covariance and Performance Analysis for Proximity Operations

4. Jang J. S. Bhatt M. Fritz and D. Woffinden. 2017. “Linear covariance analysis for a lunar lander.” In Proc. AIAA Guidance Navigation and Control Conf. 1499. Grapevine TX: American Institute of Aeronautics and Astronautics.

5. Statistical analysis of nonimpulsive orbital transfers under thrust errors;Jesus A. D. C.;Nonlinear Dyn. Syst. Theory,2012

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