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Volumn 22, Issue 3, 1999, Pages 433-440

Spacecraft vibration reduction using pulse-width pulse-frequency modulated input shaper

Author keywords

[No Author keywords available]

Indexed keywords

COMMAND AND CONTROL SYSTEMS; COMPUTER SIMULATION; DAMPING; FLEXIBLE STRUCTURES; FLIGHT SIMULATORS; MATHEMATICAL MODELS; PULSE WIDTH MODULATION; ROBUSTNESS (CONTROL SYSTEMS); SPACECRAFT;

EID: 0032635807     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4415     Document Type: Article
Times cited : (112)

References (12)
  • 2
    • 85003321467 scopus 로고
    • Limit cycle oscillations in pulse modulated systems
    • Clark, R. N., and Franklin, G. F., "Limit Cycle Oscillations in Pulse Modulated Systems," Journal of Spacecraft and Rockets, Vol. 6, No. 7, 1969, pp. 799-804.
    • (1969) Journal of Spacecraft and Rockets , vol.6 , Issue.7 , pp. 799-804
    • Clark, R.N.1    Franklin, G.F.2
  • 3
    • 0028463898 scopus 로고
    • Multiaxis tracking and attitude control of flexible spacecraft with reaction jets
    • Hablani, H. B., "Multiaxis Tracking and Attitude Control of Flexible Spacecraft with Reaction Jets," Journal of Guidance, Control, and Dynamics, Vol. 17, No. 4, 1994, pp. 831-839.
    • (1994) Journal of Guidance, Control, and Dynamics , vol.17 , Issue.4 , pp. 831-839
    • Hablani, H.B.1
  • 4
    • 0020951664 scopus 로고
    • Design of reaction jet attitude control systems for flexible spacecraft
    • Noordwijkerhout, The Netherlands, International Federation on Automatic Control, Laxemburg, Austria
    • Bittner, H., Fischer, H. D., and Surauer, M., "Design of Reaction Jet Attitude Control Systems for Flexible Spacecraft," Proceedings of the IFAC Automatic Control in Space Conference (Noordwijkerhout, The Netherlands), International Federation on Automatic Control, Laxemburg, Austria, 1982, pp. 373-398.
    • (1982) Proceedings of the IFAC Automatic Control in Space Conference , pp. 373-398
    • Bittner, H.1    Fischer, H.D.2    Surauer, M.3
  • 5
    • 0021460935 scopus 로고
    • Attitude stabilization of flexible spacecraft during stationkeeping maneuvers
    • Wie, B., and Plescia, C. T., "Attitude Stabilization of Flexible Spacecraft During Stationkeeping Maneuvers," Journal of Guidance, Control, and Dynamics, Vol. 7, No. 4, 1984, pp. 430-436.
    • (1984) Journal of Guidance, Control, and Dynamics , vol.7 , Issue.4 , pp. 430-436
    • Wie, B.1    Plescia, C.T.2
  • 6
    • 0025511526 scopus 로고
    • Pulse-modulated control synthesis for a flexible spacecraft
    • Anthony, T., Wei, B., and Carroll, S., "Pulse-Modulated Control Synthesis for a Flexible Spacecraft," Journal of Guidance, Control, and Dynamics, Vol. 13, No. 6, 1990, pp. 1014, 1015.
    • (1990) Journal of Guidance, Control, and Dynamics , vol.13 , Issue.6 , pp. 1014
    • Anthony, T.1    Wei, B.2    Carroll, S.3
  • 7
    • 23944464650 scopus 로고    scopus 로고
    • Derivation and properties of convolved and simultaneous two-mode input shapers
    • San Francisco, CA, International Federation on Automatic Control, Laxemburg, Austria
    • Crain, E., Singhose, W. E., and Seering, W. P., "Derivation and Properties of Convolved and Simultaneous Two-Mode Input Shapers," Proceedings of the 13th Triennial IFAC World Congress (San Francisco, CA), Vol. O, International Federation on Automatic Control, Laxemburg, Austria, 1996, pp. 441-446.
    • (1996) Proceedings of the 13th Triennial IFAC World Congress , vol.O , pp. 441-446
    • Crain, E.1    Singhose, W.E.2    Seering, W.P.3
  • 8
    • 0029490810 scopus 로고
    • A comparison of constant and variable amplitude command shaping techniques for vibration reduction
    • Albany, NY, Inst. of Electrical and Electronics Engineers, Piscataway, New Jersey
    • Pao, L., and Singhose, W., "A Comparison of Constant and Variable Amplitude Command Shaping Techniques for Vibration Reduction," Proceedings of the 4th IEEE Conference on Control Applications (Albany, NY), Inst. of Electrical and Electronics Engineers, Piscataway, New Jersey, 1995, pp. 1120-1125.
    • (1995) Proceedings of the 4th IEEE Conference on Control Applications , pp. 1120-1125
    • Pao, L.1    Singhose, W.2
  • 10
    • 0015022815 scopus 로고
    • Results of flexible spacecraft attitude control studies utilizing hybrid coordinates
    • Likins, P. W., and Fleischer, G. E., "Results of Flexible Spacecraft Attitude Control Studies Utilizing Hybrid Coordinates," Journal of Spacecraft and Rockets, Vol. 8, No. 3, 1971, pp. 264-273.
    • (1971) Journal of Spacecraft and Rockets , vol.8 , Issue.3 , pp. 264-273
    • Likins, P.W.1    Fleischer, G.E.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.