A Pre-Processed Orbital Parameters Approach for Improving Cubesat Orbit Propagator and Attitude Determination-Reference-Cited by-同舟云学术

A Pre-Processed Orbital Parameters Approach for Improving Cubesat Orbit Propagator and Attitude Determination

Published:2016 Issue:5 Volume:59 Page:278-286
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

GOH Shu Ting¹,CHIA Jiun Wei¹,CHIN Shi Tong¹,LOW Kay Soon¹,LIM Lip San¹

Affiliation:

1. Satellite Research Centre, School of Electrical and Electronic Engineering, Nanyang Technological University

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/59/5/59_T-15-60/_pdf

Reference20 articles.

1. 1) Goh, S. T., Lau, Z., and Low, K. S.: An Optimization Method for Nano-satellite and Pico-satellite Separation through a Two Mass-One Spring System, AAS/AIAA Astrodynamics Specialist Conference, Hilton Head, South Carolina, Aug. 2013.

2. 2) Bui, T. D. V., Low, K. S., Lau, Z., Pham, V. H. P., and Tissera, M. S. C.: System Design and Development of VELOX-I Nanosatellite, IEEE Aerospace Conference, Big Sky, Montana, March 2015.

3. 3) Xie, S. L., Lee, G. X., Low, K. S., and Gunawan, E.: Wireless Sensor Network for Satellite Applications: A Survey and Case Study, Unmanned Systems, 2 (2014), pp. 261–277.

4. 4) Qian, X. Y., Yu, H., Chen, S. S., and Low, K. S.: An Adaptive Integration Time CMOS Image Sensor with Multiple Readout Channels, IEEE Sensors J., 13 (2013), pp. 4931–4939.

5. 5) Tuthill, J.: Design and Simulation of a Nano-Satellite Attitude Determination System, Naval Postgraduate School, Monterey, CA, Dec. 2009 (Master Thesis).

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