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Volumn , Issue , 2000, Pages

Nonlinear control of satellite formation flight

Author keywords

[No Author keywords available]

Indexed keywords

DEGREES OF FREEDOM (MECHANICS); EQUATIONS OF STATE; NONLINEAR EQUATIONS; RICCATI EQUATIONS; SATELLITES;

EID: 85088758629     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-4436     Document Type: Conference Paper
Times cited : (36)

References (18)
  • 1
    • 84894479929 scopus 로고    scopus 로고
    • Available on the Web at
    • Available on the Web at http://www.vs.afrl.af.mil/factsheets /TechSat21.html
  • 2
    • 84894485302 scopus 로고    scopus 로고
    • Available on the Web at
    • Available on the Web at http://tpf.jpl.nasa.gov/mission/mission.html
  • 4
    • 0033285038 scopus 로고    scopus 로고
    • Graphs, Matrix Inequalities, and Switching for the Formation Flying Control of Multiple Spacecraft
    • San Diego, CA, June
    • Mesbahi, M. and Hadaegh, F. Y., Graphs, Matrix Inequalities, and Switching for the Formation Flying Control of Multiple Spacecraft, Proceedings of the American Controls Conference, San Diego, CA, June, 1999.
    • (1999) Proceedings of the American Controls Conference
    • Mesbahi, M.1    Hadaegh, F.Y.2
  • 5
    • 0022025257 scopus 로고
    • Formationkeeping for a Pair of Satellites in a Circular Orbit, Journal of Guidance
    • Vassar, 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) Control and Dynamics , vol.8 , Issue.2 , pp. 235-242
    • Vassar, R.H.1    Sherwood, R.B.2
  • 6
    • 0033285327 scopus 로고    scopus 로고
    • Graphs, An Adaptive Control Approach to Satellite Formation Flying with Relative Distance Constraints
    • San Diego, CA, June
    • Lawton, J., Beard, R. W. and Hadaegh, F. Y., Graphs, An Adaptive Control Approach to Satellite Formation Flying with Relative Distance Constraints, Proceedings of the American Controls Conference, San Diego, CA, June, 1999.
    • (1999) Proceedings of the American Controls Conference
    • Lawton, J.1    Beard, R.W.2    Hadaegh, F.Y.3
  • 7
    • 0033284291 scopus 로고    scopus 로고
    • Graphs, Finite Thrust Control for Satellite Formation Flying with State Constraints
    • San Diego, CA, June
    • Beard, R. W. and Hadaegh, F. Y., Graphs, Finite Thrust Control for Satellite Formation Flying with State Constraints, Proceedings of the American Controls Conference, San Diego, CA, June, 1999.
    • (1999) Proceedings of the American Controls Conference
    • Beard, R.W.1    Hadaegh, F.Y.2
  • 8
    • 0033285341 scopus 로고    scopus 로고
    • Graphs, Fuel Optimized Rotation for Satellite Formations in Free Space
    • San Diego, CA, June
    • Beard, R. W. and Hadaegh, F. Y., Graphs, Fuel Optimized Rotation for Satellite Formations in Free Space, Proceedings of the American Controls Conference, San Diego, CA, June, 1999.
    • (1999) Proceedings of the American Controls Conference
    • Beard, R.W.1    Hadaegh, F.Y.2
  • 10
    • 0031647547 scopus 로고    scopus 로고
    • 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
  • 11
    • 33645394209 scopus 로고    scopus 로고
    • Position and Attitude Control of a satellite by Sliding mode Control
    • Philadelphia, PA, June
    • Terui, F., Position and Attitude Control of a satellite by Sliding mode Control, Proceedings of the American Controls Conference, Philadelphia, PA, June, 1998.
    • (1998) Proceedings of the American Controls Conference
    • Terui, F.1
  • 12
    • 0034545266 scopus 로고    scopus 로고
    • Position and Attitude Control of a Spacecraft Using the State-Dependent Riccati Equation Technique
    • Chicago, IL, June
    • Stansbery, D. T. and Cloutier, J. R., Position and Attitude Control of a Spacecraft Using the State-Dependent Riccati Equation Technique, Accepted to the American Controls Conference, Chicago, IL, June, 2000.
    • (2000) Accepted to The American Controls Conference
    • Stansbery, D.T.1    Cloutier, J.R.2
  • 16
    • 0033349571 scopus 로고    scopus 로고
    • Control of a Continuously Stirred Tank Reactor Using an Asymmetric Solution of the State-Dependent Riccati Equation
    • HI, August
    • Cloutier, J. R. and Stansbery, D. T., Control of a Continuously Stirred Tank Reactor Using an Asymmetric Solution of the State-Dependent Riccati Equation, Proceedings of Conference on Control Applications Hawaii, HI, August, 1999.
    • (1999) Proceedings of Conference On Control Applications Hawaii
    • Cloutier, J.R.1    Stansbery, D.T.2
  • 17
    • 0033283409 scopus 로고    scopus 로고
    • Implementation of Autonomous GPS Guidance and Control for the Spacecraft Formation Flying
    • San Diego, CA, June
    • Xing, G. Q., Parvez, S. A. and Folta, D., Implementation of Autonomous GPS Guidance and Control for the Spacecraft Formation Flying, Proceedings of the American Controls Conference, San Diego, CA, June, 1999.
    • (1999) Proceedings of the American Controls Conference
    • Xing, G.Q.1    Parvez, S.A.2    Folta, D.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.