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Huang Xiang-hua (2004)
Design of Driving Scheme for Electric-driven Flight Simulator with High Power and High PrecisionJournal of Chinese Inertial Technology
J. Schwartz, M. Peck, C. Hall (2003)
Historical review of air-bearing spacecraft simulatorsJournal of Guidance Control and Dynamics, 26
D. Bernstein, N. McClamroch, A. Bloch (2001)
Development of air spindle and triaxial air bearing testbeds for spacecraft dynamics and control experimentsProceedings of the 2001 American Control Conference. (Cat. No.01CH37148), 5
Dongwon Jung, P. Tsiotras (2003)
A 3-DoF Experimental Test-Bed for Integrated Attitude Dynamics and Control Research
K. Wang, Z.L. Wang, Y. Fu, W. Li
Design and research of electronic‐hydraulic rotary‐table
Fu-sheng Wang, Gang Bao (2011)
Static characteristics of new type externally pressurized spherical air bearingsJournal of Central South University of Technology, 18
Purpose – The purpose of this paper is to develop a tri‐axis spacecraft simulator to simulate the three‐axis attitude motion of a satellite and for ground‐based hardware‐in‐the‐loop simulation. Design/methodology/approach – The structure of tri‐axis satellite attitude simulator is designed first. Full dynamic model is then derived. Based on the dynamic model, a simple proportional‐integral‐derivative controller is developed and applied to control the motion of simulator. Findings – The effectiveness of the proposed simulator configuration has been verified through numerical simulations. The tri‐axis simulator can follow the satellite attitude motion precisely. Originality/value – This paper is valuable for researchers working on the development of tri‐axis spacecraft attitude simulator. This work is original. The simulator configuration has been applied to a satellite mission that was launched successfully in 2006.
Aircraft Engineering and Aerospace Technology – Emerald Publishing
Published: Mar 23, 2010
Keywords: Spacecraft; Simulation; Aerodynamics; Control technology; Artificial satellites
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