Thermally induced attitude dynamics of a spacecraft with a flexible appendage

Journal of Guidance, Control, and Dynamics

Volumn 21, Issue 4, 1998, Pages 581-587

  Johnston, John D ^a,b   Thornton, Earl A ^a,b  

^a University of Virginia   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; DEFORMATION; DYNAMIC RESPONSE; OSCILLATIONS; THERMAL EFFECTS; TORQUE; TRANSIENTS;

FLEXIBLE APPENDAGE; LAGRANGE EQUATIONS; THERMALLY INDUCED ATTITUDE DYNAMICS;

FLEXIBLE STRUCTURES;

EID: 0032123923     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4297     Document Type: Article

References (14)

1. Thornton, E. A., Thermal Structures for Aerospace Applications, AIAA Education Series, AIAA, Reston, VA, 1996, Chap. 9.
2. Johnston, J. D., and Thornton, E. A., "An Evaluation of Thermally-Induced Structural Disturbances of Spacecraft Solar Array Structures," Proceedings of the 31st Intersociety Energy Conversion Engineering Conference, Inst. of Electrical and Electronics Engineers, Washington, DC, 1996, pp. 1-6; also Paper 96-080, Aug. 1996.
3. Boley, B. A., "Thermally Induced Vibrations of Beams," Journal of the Aeronautical Sciences, Vol. 23, No. 2, 1956, pp. 179-181.
4. Zimbelman, D. F., "Thermal Shock and Its Effect on Spacecraft Attitude Control," Ph.D. Dissertation, Dept. of Aerospace Engineering Sciences, Univ. of Colorado, Boulder, CO, Aug. 1990.
5. 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, 1996, pp. 60-68.
6. Gulick, D., and Thornton, E. A., "Thermally Induced Vibrations of an Axial Boom on a Spin-Stabilized Spacecraft," Acta Astronautica, Vol. 36, No. 3, 1995, pp. 163-176.
7. 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, 1993, pp. 438-448.
8. 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, 1995, pp. 302-311.
9. Junkins, J. L., and Kim, Y., Introduction to Dynamics and Control of Flexible Structures, AIAA Education Series, AIAA, Washington, DC, 1993, pp. 148-156.
10. Boley, B. A., and Weiner, J. H., Theory of Thermal Stresses, Wiley, New York, 1960, pp. 339-345.
11. Johnston, J. D., and Thornton, E. A., "Thermally-Induced Attitude Dynamics of a Spacecraft with a Flexible Boom," American Astronautical Society/AIAA Spaceflight Mechanics Symposium, AAS Paper 97-178, Huntsville, AL, Feb. 1997.
12. Hughes, P. C., "Attitude Dynamics of a Three-Axis Stabilized Satellite with a Large Flexible Solar Array," AIAA Paper 72-857, Aug. 1972.
13. Johnston, J. D., and Thornton, E. A., "Thermally-Induced Structural Disturbances of Rigid Panel Solar Arrays," Proceedings of the 1997 Flight Mechanics Symposium, NASA CP 3345, 1997, pp. 33-47.
14. Bainum, P. M., Hamsath, N., and Krishna, R., "The Dynamics and Control of Large Space Structures After the Onset of Thermal Shock," Acta Astronautica, Vol. 19, No. 1, 1980, pp. 1-8.