Fuzzy logic based attitude control of the spacecraft X-38 along a nominal re-entry trajectory

Author:

Wu S.-F.,Engelen C.J.H.,Chu Q.-P.,Babuška R.,Mulder J.A.,Ortega G.

Publisher

Elsevier BV

Subject

Applied Mathematics,Electrical and Electronic Engineering,Computer Science Applications,Control and Systems Engineering

Reference28 articles.

1. Bauer, F. H. (1997). Satellite formation flying using an innovative autonomous control system (AUTOCON) environment. 1997 AIAA guidance, navigation, and control conference, New Orleans, LA, part 2 (pp. 657–666).

2. Bennis, R .J. M., Chu, Q. P., Mulder, J. A., & Ortega, G. (1999). Feasibility study of a fuzzy logic based controller for rendezvous and docking of automatic transfer vehicle (ATV) to the international space station (ISS). 50th IAF congress, IAF-99-A.1.05, Amsterdam, The Netherlands, 4–8, October.

3. Berenji, H. R. (1994). Refining fuzzy logic controllers with machine learning. Technology 2003: The fourth national technology transfer conference, February, vol. 2 (pp. 3–6).

4. Daley, S., & Gill, K. F. (1987). Attitude control of a spacecraft using an extended self-organizing fuzzy logic controller. Proceedings of the institute of mechanical engineers, vol. 201 (C2, 97-106).

5. ESA/ESTEC (1999). Reference re-entry trajectory: X38 reentry to Cooper, Pedy—cycle 8. Electronic file, provided through e-mail correspondence.

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