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Attitude Agile Maneuvering Control for Spacecraft Equipped with Hybrid Actuators
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Affiliation of Author(s):航天学院

Journal:JOURNAL OF GUIDANCE CONTROL AND DYNAMICS

Key Words:CONTROL MOMENT GYROS SINGULARITY ANALYSIS SYSTEMS LOGIC LAWS

ISSN No.:0731-5090

Translation or Not:no

Date of Publication:2018-03-01

Co-author:韩锋,张世杰,hb,Chen Zhiming

Correspondence Author:wyh

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Researcher

Alma Mater:哈尔滨工业大学

Education Level:哈尔滨工业大学

Degree:Doctoral Degree in Engineering

School/Department:College of Astronautics

Discipline:Guidance, Navigation, and Control

Business Address:航天学院D11-507

Contact Information:yunhuawu@nuaa.edu.cn

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