On-board generation of three-dimensional constrained entry trajectories

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Shen, Zuojun ^a   Lu, Ping ^a  

^a IOWA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONSTRAINT THEORY; DEGREES OF FREEDOM (MECHANICS); REUSABILITY;

EQUALITY CONSTRAINTS; HIGH-FIDELITY; INEQUALITY CONSTRAINT; QUASI-EQUILIBRIUM GLIDES; REUSABLE LAUNCH VEHICLES; SEARCH PROBLEM; THREE-DEGREE OF FREEDOM (3DOF); TRAJECTORY PLANNING;

TRAJECTORIES;

EID: 85085777918     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4455     Document Type: Conference Paper

References (15)

1. Harpold, J. C., and Graves, C. A., "Shuttle En try Guidance," The Journal of the Astronautical Sciences, Vol. 37, No. 3, 1979, pp. 239-268.
2. Gamble, J. D., Cerimele, C. J., Moore, T. E., and Higgins, J., "Atmospheric Guidance Concepts for an Aeroassisted Experiment," The Journal of the Astronautical Sciences, Vol.36, No. 1-2, 1988, pp. 45-71.
3. Powell, R. W., "Six-Degree-of-Freedom Guidance and Control-Entry Analysis of the HL-20," Journal of Spacecraft and Rockets, Vol. 30, No. 5, September-October, 1993, pp. 537-542
4. Fuhry, D. P., "Adaptive Atmospheric Reentry Guidance for the Kistle K-1 Orbital Vehicle," Pro ceedings of Guidance, Navigation, and Control Conference, Denver, CO, August 14-17, 2000.
5. Zimmerman, C., Dukeman, G., and Hanson, J., "An Automated Method to Compute Orbital Entry Re-Entry Trajectories with Heating Con straints", AIAA paper 2002-4454, to be presented at the AIAA Guidance, Navigation, and Control Conference, Monterey, August 5-8, 2002
6. Mease, K. D., Chen, D. T., Teufel, P., and Schoe-Nenberger, H., "Reduced-Order Entry Trajectory Planning for Acceleration Guidance", Journal of Guidance, Control, and Dynamics, Vol. 25, No. 2, 2002, pp. 257-266.
7. Roenneke, A. J.,"Adaptive On-board Guidance for Entry Vehicle," Proceedings of the AIAA Guidance, Navigation, and Control Conference, Montreal, Canada, August 6-9, 2001.
8. Girerd, A., and Barton, G., "Next Generation En try Guidance - Onboard Trajectory Generation for Unpowered Drop Tests," Proceedings of the AIAA Guidance, Navigation, and Control Conference, Denver, CO, August 14-17, 2000.
9. Lu, P., "Regulation about Time-Varying Tra jectories: Precision Entry Guidance Illustrated," Journal of Guidance, Control, and Dynamics, Vol. 22, No. 6, 1999, pp. 784-790.
10. Vinh, N. X., Busemann, A., and Culp, R. D., Hypersonic and Planetary Entry Flight Mechanics, The University of Michigan Press, Ann Arbor, MI, 1980, pp. 26-27
11. Lu, P., "Closed-Form Control Laws for Linear Time-Varying Systems," IEEE Trans. on Auto matic Control, Vol. 45, No. 3, March 2000, pp. 537-542.
12. Shen, Z., "On-Board Three-Dimensional Con strained Entry Flight Trajectory Generation," Ph.D. Dissertation, Iowa state University, April 2002.
13. Lu, P., and Hanson, J. M., "Entry Guidance for the X-33 Vehicle," Journal of Spacecraft and Rockets, Vol. 35, No. 3, May - June 1998, pp. 342-349.
14. Hanson, J., "Advanced Guidance and Control Project for Reusable Launch Vehicles," Proceedings of Guidance, Navigation, and Control Conference, Denver, CO, August 14-17, 2000.
15. Justus, C. G. and Johnson, D. L., The NASA/MSFC Global Reference Atmospheric Model: 1999 Version (GRAM-99), NASA TM- 209630, May, 1999