메뉴 건너뛰기




Volumn 6, Issue , 2003, Pages 2587-2597

System design issuesi of formation-flying spacecraft

Author keywords

[No Author keywords available]

Indexed keywords

ACTIVE CONTROL METHODS; CLUSTER STABILITY; FORMATION FLYING; FORMATION FLYING SPACECRAFT; PERTURBATIVE FORCES; SOLAR RADIATION PRESSURE; SPACECRAFT DESIGN; STATION KEEPING;

EID: 84879375499     PISSN: 1095323X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/AERO.2003.1235185     Document Type: Conference Paper
Times cited : (6)

References (10)
  • 1
    • 0001229316 scopus 로고    scopus 로고
    • Gravitational perturbations, nonlinearity and circular orbit assumption effects on formation flying control strategies
    • Paper No. AAS 00-012, , Breckenridge, CO, Feb
    • K.T.Alfriend, H. Schaub, and D.W.Gim, "Gravitational Perturbations, Nonlinearity and Circular Orbit Assumption Effects on Formation Flying Control Strategies", Paper No. AAS 00-012, 23rd Annual A AS Guidance and Control Conference, Breckenridge, CO, Feb. 2000
    • (2000) 23rd Annual A AS Guidance and Control Conference
    • Alfriend, K.T.1    Schaub, H.2    Gim, D.W.3
  • 2
    • 0008786705 scopus 로고    scopus 로고
    • Time-explicit representation of relative motion between elliptical orbits
    • Sunvalley, ID, Aug
    • R.G. Melton, "Time-Explicit representation of relative Motion Between Elliptical Orbits," AAS/AL4A Astrodynamics Specialists Conference, Sunvalley, ID, Aug. 1997
    • (1997) AAS/AL4A Astrodynamics Specialists Conference
    • Melton, R.G.1
  • 3
    • 1542297467 scopus 로고    scopus 로고
    • Low-cost, minimum-size satellites for demonstration of formation flying modes at small, kilometer-size distances
    • Hans.F.Meissinger, "Low-cost, minimum-size satellites for demonstration of formation flying modes at small, kilometer-size distances," 13th AIAA/USU Conference on Small Satellites, 1999
    • (1999) 13th AIAA/USU Conference on Small Satellites
    • Meissinger, H.F.1
  • 4
    • 0035729987 scopus 로고    scopus 로고
    • The state transition matrix of relative motion for the perturbed non-circular reference orbit
    • Feb. 11-16, 2001, Santa Barbara
    • D.W.Gim, and K.T. Alfriend., "The State Transition Matrix of Relative Motion for the Perturbed Non-Circular Reference Orbit", 2001 AAS/AL4A Space Flight Mechanics Meeting, Feb. 11-16, 2001, Santa Barbara
    • (2001) AAS/AL4A Space Flight Mechanics Meeting
    • Gim, D.W.1    Alfriend, K.T.2
  • 6
    • 0034818720 scopus 로고    scopus 로고
    • Satellite clusters with constant apparent distribution
    • Jan.-Feb
    • David F. Chichka, " Satellite Clusters with Constant Apparent Distribution", Journal of Guidance, Control, and Dynamics, Vol. 24, No. 1. Jan.-Feb. 2001
    • (2001) Journal of Guidance, Control, and Dynamics , vol.24 , Issue.1
    • Chichka, D.F.1
  • 7
    • 0024305185 scopus 로고
    • Orbital formation-keeping with differential drag
    • Jan.-Feb
    • C.L.Leonard, " Orbital Formation-Keeping with Differential Drag", Journal of Guidance, Control, and Dynamics, Vol. 12, No. 1. Jan.-Feb. 1989
    • (1989) Journal of Guidance, Control, and Dynamics , vol.12 , Issue.1
    • Leonard, C.L.1
  • 8
    • 0003738441 scopus 로고
    • An introduction to the mathematics and methods of astrodynamics
    • Washington D.C
    • R.H.Battin, " An introduction to the Mathematics and Methods of Astrodynamics", AIAA Education series, Washington D.C. 1987
    • (1987) AIAA Education Series
    • Battin, R.H.1
  • 10
    • 0041160938 scopus 로고    scopus 로고
    • Potential uses of solar radiation pressure in satellite formation flight
    • Clearwater, FL, Jan
    • T.W. Williams and Z. S. Wang, "Potential Uses of Solar Radiation Pressure in Satellite Formation Flight", 10th AAS/AIAA Space Flight Mechanics Meeting, Clearwater, FL, Jan. 2000
    • (2000) 10th AAS/AIAA Space Flight Mechanics Meeting
    • Williams, T.W.1    Wang, Z.S.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.