Multibody dynamics of parachute and balloon flight systems for planetary exploration

Journal of Guidance, Control, and Dynamics

Volumn 27, Issue 4, 2004, Pages 564-571

  Quadrelli, Marco B ^a,b   Cameron, Jonathan M ^a,b   Kerzhanovich, Viktor ^a,c  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^b Autonomy and Control Section   (United States)

^c Avionic Systems Engineering Section   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BALLOONS; COMPUTER SIMULATION; CONTROL THEORY; EQUATIONS OF MOTION; INTERPLANETARY SPACECRAFT; MATHEMATICAL MODELS; PARACHUTES; PERTURBATION TECHNIQUES; SENSORS; SPACE FLIGHT; SYSTEM STABILITY;

FLIGHT STABILITY; PAYLOADS; PLANETARY EXPLORATION;

FLIGHT DYNAMICS;

EID: 3843078483     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.11374     Document Type: Article

References (14)

1. Kerzhanovich, V. V., Cutts, J., Bachelder, A., Cameron, J., Hall, J., Patzold, J., Yavrouian, A., Cantrell, J., and Lachenmeier, T., "Mars Aerobot Validation Program," Proceedings of the AIAA International Balloon Technology Conference, AIAA, Reston, VA, 1999, pp. 8-20.
2. Quadrelli, M., Cameron, J., and Kerzhanovieh, V., "Modeling, Simulation, and Control of Parachute/Balloon Flight Systems for Mars Exploration," AIAA Paper 2001-2026, May 2001.
3. Kerzhanovich, V. V., Cutts, J. A., Bachelder, A. D., Cameron, J. M., Hall, J. L., Quadrelli, B. M., Patzold, J. D., Yavrouian, A. H., Cantrell, J. A., and Lachenmeier, T. T., "MABVAP - One Step Closer to an Aerobot Mission to Mars," 5th International Conference on Mars, Paper 16, The Lunar and Planetary Inst., July 1999.
4. Ash, R., "Balloon Concepts for Scientific Investigation of Mars and Jupiter," Proceedings of the AIAA 6th Aerodynamic Decelerator and Balloon Technology Conference, AIAA, New York, 1979, pp. 26-37.
5. Carten, A., and Wuest, M., "The Air-Launched Balloon System Phase II Design Improvement and Test Program," 7th AIAA Aerodynamic Decelerator Systems Technology Conference, AIAA Paper 81-1930, 1981.
6. Romero, M., Rougerch, M., and Tockert, C., "Thermal Balance of Pumpkin Shaped Balloons and Its Relation with IR Earth Radiation," 7th AIAA Aerodynamic Decelerator Systems Technology Conference, AIAA Paper 81-1938, 1981.
7. Vargas, A., Tarrieu, C., Lepage, J. P., Mauoy, P., and Sirmain, C., "Mars Balloon Simulator," Paper 91-436, International Astronautical Federation Conf., Oct. 1991.
8. Dowell, E. H. (ed.), A Modern Course in Aeroelasticity, 3rd ed., Kluwer Academic Publishers, Norwell, MA, 1995, Chap. 6.1.
9. Cockrell, D. J., and Young, A. D.,Aerodynamics of Parachutes, AGARD-ograph 295, AGARD, 1987.
10. Ewing, E. G., Bixby, H. W., and Knacke, T. W., "Recovery System Design Guide," Air Force Flight Dynamics Lab., AFDL-TR-78-151, Dec. 1978.
11. Knacke, T. W., Parachute Recovery Systems Design Manual, Naval Warfare Center, NWC TP-6575, March 1992.
12. Kurdila, A., "Multibody Dynamics Formulations Using Maggi's Approach," Mechanics and Control of Large Space Structures, edited by J. L. Junkins, Progress in Aeronautics and Astronautics Series, Vol. 129, AIAA, Washington, DC, 1990, Chap. 6.
13. Neimark, J. I., and Fufaev, N. A., Dynamics of Nonholonomic Systems, American Mathematical Society, Mathematical Monograph 33, Providence, RI, 1972, Chap. 4.
14. MATLAB, ver. 5.3, The Mathworks, Inc., Natick, MA, 1999.