Fault-Tolerant Attitude Determination and Control System Design of Nanosatellite 2-Reference-Cited by-同舟云学术

Fault-Tolerant Attitude Determination and Control System Design of Nanosatellite 2

Published:2018-11 Issue:6 Volume:31 Page:04018087
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Shi Shuai¹,Yuan Binwen¹,Zhao Kaichun²,You Zheng³,Zhang Gaofei⁴

Affiliation:

1. Graduate Student, State Key Laboratory of Precision Measurement Technology and Instruments, Dept. of Precision Instrument, Tsinghua Univ., Beijing 100084, P.R. China.

2. Associate Professor, State Key Laboratory of Precision Measurement Technology and Instruments, Dept. of Precision Instrument, Tsinghua Univ., Beijing 100084, P.R. China (corresponding author).

3. Professor, State Key Laboratory of Precision Measurement Technology and Instruments, Dept. of Precision Instrument, Tsinghua Univ., Beijing 100084, P.R. China.

4. Associate Professor, State Key Laboratory of Precision Measurement Technology and Instruments, Dept. of Precision Instrument, Tsinghua Univ., Beijing 100084, P.R. 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.1943-5525.0000912

Reference25 articles.

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2. Berkovitz D. E. Kong D. Miller 2003. “System identification of the SPHERES autonomous rendezvous and docking testbed.” In Vol. 49 of Proc. AIAA Space 2003 Conf. and Exposition 135–139. Reston VA: ASCE.

3. Survey of worldwide pico- and nanosatellite missions, distributions and subsystem technology

4. Active Fault-Tolerant Control of UAV Dynamics against Sensor-Actuator Failures

5. International Geomagnetic Reference Field: the eleventh generation

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