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Volumn 31, Issue 3, 2003, Pages 257-274

Optimal control of deployment of a tethered subsatellite

Author keywords

Pontrijagin's Maximum Principle; State constraint; Time optimal solution

Indexed keywords

EARTH (PLANET); GRAVITATION; MAGNETIC FIELDS; MAXIMUM PRINCIPLE; OPTIMAL CONTROL SYSTEMS; ORBITS; OSCILLATIONS; SPACE SHUTTLES; TENSILE STRENGTH; TETHERLINES;

EID: 0037305291     PISSN: 0924090X     EISSN: None     Source Type: Journal    
DOI: 10.1023/A:1022956002484     Document Type: Article
Times cited : (88)

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  • 2
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  • 16
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    • Reihe B, Bericht 13
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    • (1984) Numerical Methods for Bifurcation Problems , pp. 480-494
    • Seydel, R.1
  • 19
    • 0001927055 scopus 로고
    • Dynamics of a space tethered satellite system with two rigid endbodies
    • (ed.), Science and Technology Corporation, Hampton, VA
    • Steiner, W., Steindl, A., and Troger, H., 'Dynamics of a space tethered satellite system with two rigid endbodies', in Proceedings of the Fourth International Conference on Tethers in Space, (ed.), Science and Technology Corporation, Hampton, VA, 1995, pp. 1367-1379.
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  • 20
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    • Center manifold approach to the control of a tethered satellite system
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.