2024-03-28T13:25:36Z
https://soar-ir.repo.nii.ac.jp/oai
oai:soar-ir.repo.nii.ac.jp:00018380
2022-12-14T04:00:57Z
1221:1222
Nonlinear Tracking Control of Rigid Spacecraft under Disturbance using PID-type H-infinity Adaptive State Feedback
Ikeda, Yuichi
Kida, Takashi
Nagashio, Tomoyuki
Spacecraft
Tracking Control
PID-type H-infinity Adaptive State Feedback Control
Future space programs will require an agile relative position and attitude control technology for spacecraft. Rendezvous and docking, capture of inoperative spacecraft and formation flight in orbit are the typical scenarios. One of the key technologies is designing the tracking controllers that can control the six degrees-of-freedom (d.o.f.) of spacecraft under the influence of physical parameter uncertainties and external disturbances. To achieve agility, the controller design must be formulated as nonlinear control problems where translational and rotational motions are dynamically coupled with each other. This paper proposes a tracking controller, proportional-integral-derivative (PID)-type H-infinity adaptive state feedback controller, that can attenuate disturbances. The proposed controller has positive definite gain matrices whose conditions to be satisfied are given by linear matrix inequalities. The properties of the proposed controller were evaluated through numerical studies and compared with those of existing controllers.
Article
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 58(5):289-297 (2015)
journal article
JAPAN SOC AERONAUT SPACE SCI
2015-09-01
application/pdf
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
5
58
289
297
0549-3811
AA10679655
https://soar-ir.repo.nii.ac.jp/record/18380/files/Nonlinear_Tracking_Control_Rigid_Spacecraft.pdf
eng
10.2322/tjsass.58.289
https://doi.org/10.2322/tjsass.58.289
Copyright © 2015 The Japan Society for Aeronautical and Space Sciences