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Volumn 112 II, Issue , 2002, Pages 1063-1080

Application of several control techniques for the ionospheric observation nanosatellite formation

Author keywords

[No Author keywords available]

Indexed keywords

COMMAND AND CONTROL SYSTEMS; COMPUTER SIMULATION; CONSTRAINT THEORY; IONOSPHERE; LINEAR CONTROL SYSTEMS; MATRIX ALGEBRA; NONLINEAR CONTROL SYSTEMS; PERTURBATION TECHNIQUES; REDUNDANCY; SPACE FLIGHT;

EID: 0036910258     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (36)

References (31)
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  • 8
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    • Vadali, S.1    Vaddi, S.2
  • 9
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    • Optimal configurations for rotating spacecraft formations
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    • Hughes, S.P.1    Hall, C.D.2
  • 10
    • 0035394681 scopus 로고    scopus 로고
    • Impulsive spacecraft formation flying control to establish specific mean orbit elements
    • Schaub, H. and Alfriend, K. T., "Impulsive Spacecraft Formation Flying Control to Establish Specific Mean Orbit Elements," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 4, 2001, pp. 739-745.
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    • Schaub, H.1    Alfriend, K.T.2
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    • Formationkeeping for a pair of satellites in a circular orbit
    • Vasser, R. H. and Sherwood, R. B., "Formationkeeping for a Pair of Satellites in a Circular Orbit," Journal of Guidance, Control, and Dynamics, Vol. 8, No. 2, 1985, pp. 235-242.
    • (1985) Journal of Guidance, Control, and Dynamics , vol.8 , Issue.2 , pp. 235-242
    • Vasser, R.H.1    Sherwood, R.B.2
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    • Long-term formation keeping of satellite constellation using linear-quadratic controller
    • Ulybyshev, Y., "Long-Term Formation Keeping of Satellite Constellation Using Linear-Quadratic Controller," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 1, 1998, pp. 109-115.
    • (1998) Journal of Guidance, Control, and Dynamics , vol.21 , Issue.1 , pp. 109-115
    • Ulybyshev, Y.1
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    • A feedback guidance scheme for orbital rendezvous
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    • (1999) Journal of the Astronautical Sciences , vol.47 , Issue.3-4 , pp. 229-237
    • Kluever, C.A.1    Tanck, G.S.2
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    • Terminal guidance system for satellite rendezvous
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    • Schaub, H. Vadali, S. R. Junkins, J. L., and Alfriend, K. T., "Spacecraft Formation Flying Control Using Mean Orbital Elements," Advances in the Astronautical Sciences, Vol. 103, Part 1, 1999, pp. 163-181, AAS 99-310.
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  • 29
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.