Attitude stabilization and test validation of underactuated post-capture combination with multiple disturbances
Author:
Affiliation:
1. National Key Laboratory of Aerospace Flight Dynamics, Xi’an, Shaanxi, PR China
2. School of Astronautics, Northwestern Polytechnical University, Xi’an, PR China
3. China Academy of Space Technology, Beijing, PR China
Abstract
Funder
Chinese National Science Foundation
Innovation Foundation for Doctor Dissertation of Northwestern Polytechnical University
Publisher
SAGE Publications
Subject
Instrumentation
Link
http://journals.sagepub.com/doi/pdf/10.1177/0142331218805146
Reference35 articles.
1. Nonlinear Attitude Control of Spacecraft with a Large Captured Object
2. Nonlinear Tracking Control of an Underactuated Spacecraft
3. Global asymptotic stabilization of the attitude and the angular rates of an underactuated non-symmetric rigid body
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