Near-minimum-fuel Strategy for Continuous Single-axis Maneuvers of a Rigid Body-Reference-Cited by-同舟云学术

Near-minimum-fuel Strategy for Continuous Single-axis Maneuvers of a Rigid Body

Published:2019 Issue:3 Volume:62 Page:169-172
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

KIM Donghoon¹,LEEGHIM Henzeh²

Affiliation:

1. Department of Aerospace Engineering, Mississippi State University

2. Department of Aerospace Engineering, Chosun University

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/62/3/62_T-18-39/_pdf

Reference10 articles.

1. 1) Junkins, J. L. and Turner, J. D.: Optimal Continuous Torque Attitude Maneuvers, J. Guid. Control Dynam., 3 (1980), pp. 210–217.

2. 2) Seywald, H., Kumar, R. R., Deshpande, S. S., and Heck, M. L.: Minimum Fuel Spacecraft Reorientation, J. Guid. Control Dynam., 17 (1994), pp. 21–29.

3. 3) Junkins, J. L., Rahman, Z. H., and Bang, H.: Near-Minimum-Time Control of Distributed Parameter Systems: Analytical and Experimental Results, J. Guid. Control Dynam., 14 (1991), pp. 406–415.

4. 4) Thompson, R. C., Junkins, J. L., and Vadali, S. R.: Near-Minimum-Time, Open-Loop Slewing of Flexible Vehicles, J. Guid. Control Dynam., 12 (1989), pp. 82–88.

5. 5) Byers, R. M., Vadali, S. R., and Junkins, J. L.: Near-Minimum-Time, Closed-Loop Slewing of Flexible Spacecraft, J. Guid. Control Dynam., 13 (1990), pp. 57–65.

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