Novel Approach to Determine Spinning Satellites’ Attitude by RCS Measurements-Reference-Cited by-同舟云学术

Novel Approach to Determine Spinning Satellites’ Attitude by RCS Measurements

Published:2021-07 Issue:4 Volume:34 Page:04021023
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Lyu Jiang-Tao¹,Zhong Wei-Jun²,Liu Hong³,Geng Yan⁴,Ben De⁵

Affiliation:

1. Professorate Senior Engineer, School of Electronic Science and Engineering, Nanjing Univ., No. 163 Xianlin Ave., Qixia District, Nanjing, Jiangsu Province 210023, China; Nanjing Research Institute of Electronics Technology, No. 8 Guorui Rd., Yuhuatai District, Nanjing, Jiangsu Province 210039, China (corresponding author).

2. Director, School of Automation, Northwestern Polytechnical Univ., No. 127 Friendship Rd., Beilin District, Xi’an, Shanxi Province 710021, China; China State Key Laboratory of Astronautic Dynamics, No. 462-15, Xianning East Rd., Xincheng District, Xi’an, Shanxi Province 710043, China.

3. China State Key Laboratory of Astronautic Dynamics, No. 462-15, Xianning East Rd., Xincheng District, Xi’an, Shanxi Province 710043, China.

4. Master, China State Key Laboratory of Astronautic Dynamics, No. 462-15, Xianning East Rd., Xincheng District, Xi’an, Shanxi Province 710043, China.

5. Academician of Chinese Academy of Engineering, Professorate Senior Engineer, Nanjing Research Institute of Electronics Technology, No. 8 Guorui Rd., Yuhuatai District, Nanjing, Jiangsu Province 210039, 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.1943-5525.0001253

Reference22 articles.

1. Measurement of spatial object’s exterior attitude based on linear CCD

2. EFFECT OF ATMOSPHERIC PROPAGATION IN RCS PREDICTIONS

3. Buthainah A. K. and K.-M. Chilukuri. 2002. “Multi-phase discrete particle swarm optimization.” In Proc. 4th Int. Workshop on Frontiers in Evolutionary Algorithms. Lausanne Switzerland: Frontiers.

4. Crassidis J. L. S. F. Andrews F. L. Markley and K. Ha. 1995. “Contingency designs for attitude determination of TRMM.” In Proc. Flight Mechanics/Estimation Theory Symp. 419–433. Washington DC: National Aeronautics and Space Administration.

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