메뉴 건너뛰기




Volumn 95 PART 2, Issue , 1997, Pages 975-989

Thermally-induced attitude dynamics of a spacecraft with a flexible boom

Author keywords

[No Author keywords available]

Indexed keywords


EID: 5744242888     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article
Times cited : (2)

References (28)
  • 1
    • 5744239380 scopus 로고
    • Effects of Structural Flexibility on Spacecraft Control Systems
    • NASA SP-8016, April
    • Effects of Structural Flexibility on Spacecraft Control Systems, NASA Space Vehicle Design Criteria (Guidance and Control), NASA SP-8016, April 1969.
    • (1969) NASA Space Vehicle Design Criteria (Guidance and Control)
  • 2
    • 0000084797 scopus 로고
    • Dynamic Response of Rapidly Heated Space Structures
    • Edited by S.N. Alturi, Progress in Astronautics and Aeronautics, AIAA, Washington, DC
    • Thornton, E.A. and Foster, R.S., "Dynamic Response of Rapidly Heated Space Structures," Computational Nonlinear Mechanics in Aerospace Engineering, Edited by S.N. Alturi, Vol. 146, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 1992, pp. 451-477.
    • (1992) Computational Nonlinear Mechanics in Aerospace Engineering , vol.146 , pp. 451-477
    • Thornton, E.A.1    Foster, R.S.2
  • 4
    • 0001501982 scopus 로고
    • Thermally Induced Vibrations of Beams
    • Feb.
    • Boley, B.A., "Thermally Induced Vibrations of Beams," Journal of the Aeronautical Sciences, Vol. 23, No. 2, Feb. 1956, pp. 179-181.
    • (1956) Journal of the Aeronautical Sciences , vol.23 , Issue.2 , pp. 179-181
    • Boley, B.A.1
  • 6
    • 85003220350 scopus 로고
    • Thermally Induced Vibration and Flutter of a Flexible Boom
    • August
    • Yu, Y.Y., "Thermally Induced Vibration and Flutter of a Flexible Boom," Journal of Spacecraft and Rockets, Vol. 6, No. 8, August 1969, pp. 902-910.
    • (1969) Journal of Spacecraft and Rockets , vol.6 , Issue.8 , pp. 902-910
    • Yu, Y.Y.1
  • 7
    • 85003229294 scopus 로고
    • Variational Equation of Motion for Coupled Flexure and Torsion of Bars of Thin-Walled Open Section Including Thermal Effect
    • June
    • Yu, Y.Y., "Variational Equation of Motion for Coupled Flexure and Torsion of Bars of Thin-Walled Open Section Including Thermal Effect," Journal of Applied Mechanics, Vol. 38, No. 2, June 1971, pp.502-506.
    • (1971) Journal of Applied Mechanics , vol.38 , Issue.2 , pp. 502-506
    • Yu, Y.Y.1
  • 9
    • 84880921596 scopus 로고
    • Experimental Investigation of Thermally Induced Vibrations of Spacecraft Structures
    • Edited by E.A. Thornton, Progress in Astronautics and Aeronautics, AIAA, Washington, DC
    • Foster, R.S. and Thornton, E.A., "Experimental Investigation of Thermally Induced Vibrations of Spacecraft Structures," Aerospace Thermal Structures and Materials for a New Era, Edited by E.A. Thornton, Vol. 168, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 1995, pp. 163-177.
    • (1995) Aerospace Thermal Structures and Materials for a New Era , vol.168 , pp. 163-177
    • Foster, R.S.1    Thornton, E.A.2
  • 10
    • 0029349543 scopus 로고
    • Thermally Induced Vibrations of an Axial Boom on a Spin-Stabilized Spacecraft
    • and AIAA Paper 94-1556, April
    • Gulick, D. W. and Thornton, E.A., "Thermally Induced Vibrations of an Axial Boom on a Spin-Stabilized Spacecraft," Acta Astronautica, Vol. 36, No. 3, pp. 163-176, and AIAA Paper 94-1556, April 1994.
    • (1994) Acta Astronautica , vol.36 , Issue.3 , pp. 163-176
    • Gulick, D.W.1    Thornton, E.A.2
  • 11
    • 0027627938 scopus 로고
    • Thermally Induced Bending Vibrations of a Flexible Rolled-Up Solar Array
    • July-August
    • Thornton, E. A. and Kim, Y. A., "Thermally Induced Bending Vibrations of a Flexible Rolled-Up Solar Array," Journal of Spacecraft and Rockets, Vol. 30, No. 4, July-August 1993, pp. 438-448.
    • (1993) Journal of Spacecraft and Rockets , vol.30 , Issue.4 , pp. 438-448
    • Thornton, E.A.1    Kim, Y.A.2
  • 12
    • 0029679341 scopus 로고    scopus 로고
    • Thermal Response of Radiantly Heated Spinning Spacecraft Booms
    • and AIAA paper 95-2019
    • Johnston, J. D. and Thornton, E. A., "Thermal Response of Radiantly Heated Spinning Spacecraft Booms," Journal of Thermophysics and Heat Transfer, Vol. 10, No. 1, pp. 60-68, and AIAA paper 95-2019.
    • Journal of Thermophysics and Heat Transfer , vol.10 , Issue.1 , pp. 60-68
    • Johnston, J.D.1    Thornton, E.A.2
  • 13
    • 0029277548 scopus 로고
    • Thermally-Induced Vibrations of a Self-Shadowed Split Blanket Solar Array
    • March-April
    • Thornton, E. A., Chini, G. P., and Gulick, D. W., "Thermally-Induced Vibrations of a Self-Shadowed Split Blanket Solar Array," Journal of Spacecraft and Rockets, Vol. 32, No. 2, March-April 1995, pp. 302-311.
    • (1995) Journal of Spacecraft and Rockets , vol.32 , Issue.2 , pp. 302-311
    • Thornton, E.A.1    Chini, G.P.2    Gulick, D.W.3
  • 14
    • 0003415713 scopus 로고    scopus 로고
    • AIAA Education Series, American Institute of Aeronautics and Astronautics, Inc., Washington, D.C.
    • Thornton, E.A., Thermal Structures for Aerospace Applications, AIAA Education Series, American Institute of Aeronautics and Astronautics, Inc., Washington, D.C., 1996.
    • (1996) Thermal Structures for Aerospace Applications
    • Thornton, E.A.1
  • 15
    • 85007721208 scopus 로고
    • Modal Method for Analysis of Free Rotations of Spacecraft
    • July
    • Likins, P.W., "Modal Method for Analysis of Free Rotations of Spacecraft," AIAA Journal, Vol. 5, July, 1967, pp.1304-1308.
    • (1967) AIAA Journal , vol.5 , pp. 1304-1308
    • Likins, P.W.1
  • 16
    • 85007724398 scopus 로고
    • Use of Synthetic Modes in Hybrid Coordinate Dynamic Analysis
    • October
    • Likins, P.W. and Wirsching, P.H., "Use of Synthetic Modes in Hybrid Coordinate Dynamic Analysis," AIAA Journal, Vol. 6, No. 10, October, 1968, pp. 1867-1872.
    • (1968) AIAA Journal , vol.6 , Issue.10 , pp. 1867-1872
    • Likins, P.W.1    Wirsching, P.H.2
  • 17
    • 0015022815 scopus 로고
    • Results of Flexible Spacecraft Attitude Control Studies Using Hybrid Coordinates
    • March
    • Likins, P.W. and Fleischer, G.E., "Results of Flexible Spacecraft Attitude Control Studies Using Hybrid Coordinates," Journal of Spacecraft and Rockets, Vol. 8, No. 3, March 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
  • 18
    • 0016127311 scopus 로고
    • Attitude Dynamics of Satellites with Flexible Appendages - A Brief Review
    • Nov.
    • Modi, V.J., "Attitude Dynamics of Satellites with Flexible Appendages - A Brief Review," Journal of Spacecraft and Rockets, Vol. 11, No. 11, Nov., 1974, pp. 743-751.
    • (1974) Journal of Spacecraft and Rockets , vol.11 , Issue.11 , pp. 743-751
    • Modi, V.J.1
  • 19
    • 85003272549 scopus 로고
    • Explicit Generalization of Lagrange's Equations for Hybrid Coordinate Dynamical Systems
    • Nov.-Dec.
    • Lee, S. and Junkins, J.L., "Explicit Generalization of Lagrange's Equations for Hybrid Coordinate Dynamical Systems," Journal of Guidance, Navigation, and Control, Vol. 15, No. 6, Nov.-Dec., 1992, pp.1443-1452.
    • (1992) Journal of Guidance, Navigation, and Control , vol.15 , Issue.6 , pp. 1443-1452
    • Lee, S.1    Junkins, J.L.2
  • 20
    • 85003340103 scopus 로고
    • Optimal Large-Angle Rotational Maneuvers of Flexible Spacecraft
    • Nov.-Dec.
    • Turner, J.D. and Junkins, J.L., "Optimal Large-Angle Rotational Maneuvers of Flexible Spacecraft," Journal of Guidance and Control, Vol. 3, No. 6, Nov.-Dec., 1980, pp. 578-585.
    • (1980) Journal of Guidance and Control , vol.3 , Issue.6 , pp. 578-585
    • Turner, J.D.1    Junkins, J.L.2
  • 21
    • 85003348872 scopus 로고
    • Momentum Exchange: Feedback Control of Flexible Spacecraft Maneuvers and Vibration
    • Nov.-Dec.
    • Li, Z. and Bainum, P.M., "Momentum Exchange: Feedback Control of Flexible Spacecraft Maneuvers and Vibration," Journal of Guidance, Control, and Dynamics, Vol. 15, No. 6, Nov.-Dec., 1992, pp.1354-1136.
    • (1992) Journal of Guidance, Control, and Dynamics , vol.15 , Issue.6 , pp. 1354-11136
    • Li, Z.1    Bainum, P.M.2
  • 22
    • 0027695482 scopus 로고
    • Invariant Set Analysis of the Hub-Appendage Problem
    • Nov.-Dec.
    • Mukherjee, R. and Junkins, J.L., "Invariant Set Analysis of the Hub-Appendage Problem," Journal of Guidance, Control, and Dynamics, Vol. 16, No. 6, Nov.-Dec., 1992, pp.1191-1193.
    • (1992) Journal of Guidance, Control, and Dynamics , vol.16 , Issue.6 , pp. 1191-1193
    • Mukherjee, R.1    Junkins, J.L.2
  • 23
    • 0016494657 scopus 로고
    • Thermally Induced Nutational Body Motions of a Spinning Spacecraft with Flexible Appendages
    • April
    • Tsuchiya, K., "Thermally Induced Nutational Body Motions of a Spinning Spacecraft with Flexible Appendages," AIAA Journal, April 1975, pp.448-453.
    • (1975) AIAA Journal , pp. 448-453
    • Tsuchiya, K.1
  • 24
    • 5744225600 scopus 로고    scopus 로고
    • Dynamics of Gravity Oriented Satellites with Thermally Flexed Appendages
    • Ng, A.C. and Modi, V.J., "Dynamics of Gravity Oriented Satellites with Thermally Flexed Appendages," Astrodynamics 1987, Advances in the Astronautical Sciences, Vol. 65, Pt. 1, pp.387-410.
    • Astrodynamics 1987, Advances in the Astronautical Sciences , vol.65 , Issue.1 PART , pp. 387-410
    • Ng, A.C.1    Modi, V.J.2
  • 27
    • 0347959633 scopus 로고
    • Astro Aerospace Corporation, Carpinteria, CA, September
    • Anon., "STEM Design Characteristics and Parameters," Astro Aerospace Corporation, Carpinteria, CA, September 1985.
    • (1985) STEM Design Characteristics and Parameters


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.