Comparison of analytical modeling of OEDIPUS tethers with data from tether laboratory

Journal of Guidance, Control, and Dynamics

Volumn 20, Issue 3, 1997, Pages 471-478

  Vigneron, F R ^a,d   Jablonski, A M ^a,d   Chandrashaker, R ^a,d,e   Bergmans, J L ^b,d,f   McClure, B A ^b,g   Tyc, G ^c,d  

^a CANADIAN SPACE AGENCY   (Canada)

^b CARLETON UNIVERSITY   (Canada)

^c Bristol Aerospace Limited   (Canada)

^d AIAA   (United States)

^e PRATT AND WHITNEY CANADA   (Canada)

^f CFD RESEARCH CORPORATION   (United States)

^g Positioning Mechanisms Hughes S   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EIGENVALUES AND EIGENFUNCTIONS; FAST FOURIER TRANSFORMS; FLIGHT DYNAMICS; MATHEMATICAL MODELS; MATRIX ALGEBRA; PARAMETER ESTIMATION; PLASMAS; SYSTEM STABILITY;

TETHER LABORATORY DEMONSTRATION FACILITY (TELAB);

TETHERLINES;

EID: 0031143338     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4065     Document Type: Review

References (12)

1. Tyc, G., and Man, R. P. S., "Attitude Dynamics Investigation of the OEDIPUS-A Tethered Rocket Payload," Journal of Spacecraft and Rockets, Vol. 32, No. 1, 1995, pp. 133-141.
2. Tyc, G., Vigneron, F. R., and Jablonski, A. M., "Tether Dynamics Investigations for the Canadian OEDIPUS and BICEPS Missions," International Round Table on Tethers in Space, European Space Agency/European Space Research and Technology Center, ESA WPP-081, Noordwijk, The Netherlands, Sept. 1994.
3. Tyc, G., Han, R. P. S., Vigneron, F. R., Jablonski, A. M., Modi, V. J., and Misra, A. K., "Dynamics and Stability of a Spinning Tethered Spacecraft with Spinning Flexible Appendages," Advances in the Astronautical Sciences 1993, Vol. 85, Univelt, San Diego, CA, 1994, pp. 877-896 (AAS 93-736).
4. Han, R. P. S., "Resonant Conditions for a Stretched Spinning Tether," 4th International Conference on Tethers in Space (Washington, DC), Science and Technology Corp., Hampton, VA, 1995, pp. 1325-1340.
5. Misra, A. K., "Dynamics of Low-Tension Spinning Tethers," 4th International Conference on Tethers in Space (Washington, DC), Science and Technology Corp., Hampton, VA, 1995, pp. 1309-1324.
6. Jablonski, A. M., Vigneron, F. R., Chandrashaker, R., Bergmans, J. L., McClure, B., Staley, D. A., and Tyc, G., "Tether Laboratory Demonstration System (TE-LAB) - A Ground Test Facility For The OEDIPUS Tether Missions," 4th International Conference on Tethers in Space (Washington, DC), Science and Technology Corp., Hampton, VA, 1995,pp. 1809-1822.
7. McClure, B. A., "The Tether Laboratory Demonstration System (TE-LAB) - Design, Operation, and Mathematical Model Validation Using an Eigenvalue Approach," M.S. Thesis, Mechanical and Aerospace Engineering Dept., Carleton Univ., Ottawa, ON, Canada, March 1995.
8. Bergmans, J. L., "Tether Laboratory Demonstration System (TE-LAB); Payload Orientation Determination System, Rotation Rate Control, and Validation of Stability Criteria," M.S. Thesis, Mechanical and Aerospace Engineering Dept., Carleton Univ., Ottawa, ON, Canada, March 1995.
9. Vigneron, F. R., Jablonski, A. M., and Chandrashaker, R., "Tether Dynamics Model For The Tether Laboratory Demonstration System (TE-LAB)," Canadian Space Agency, CSA TR OED-TR-93-05, St. Hubert, PQ, Canada, Nov. 1993.
10. Vigneron, F. R., "A Natural Modes Model and Modal Identities for Damped Linear Structures," Journal of Applied Mechanics, Vol. 53, March 1986, pp. 33-38.
11. Hughes, P. C., Spacecraft Attitude Dynamics, Wiley, New York, 1986, pp. 510-520.
12. Eliuk, W., Walkty, I., Rob, R., Rumbold, G., and James, H. G., "OEDIPUS-C Tethered Suborbital Mission Description and Flight Performance," Proceedings of the 9th CASI Conference on Astronautics, Canadian Aeronautics and Space Inst., Ottawa, ON, Canada, 1996, pp. 332-341.