The X-43A Hyper-X mach 7 flight 2 guidance, navigation, and control overview and flight test results

A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn 1, Issue , 2005, Pages 682-704

  Bahm, Catherine ^a,d   Baumann, Ethan ^a,d   Martin, John ^b,d   Bose, David ^c,d   Beck, Roger E ^c,d   Strovers, Brian ^c,d  

^a NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c ANALYTICAL MECHANICS ASSOCIATES   (United States)

^d MS 4840D ^*

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEMS; HYPERSONIC AERODYNAMICS; LAUNCHING; MANEUVERABILITY; NAVIGATION; TRAJECTORIES;

ENGINE TESTS; FLIGHT CONTROL; HYPERSONIC VEHICLES; RESEARCH VEHICLES;

FLIGHT DYNAMICS;

EID: 29044435179     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. McClinton, C. R., Rausch, D. R., Sitz, J., and Reukauf, P., "Hyper-X Program Status," AIAA/NAL-NASDA-ISAS 10th International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto, Japan, AIAA 2001-1910, April 24-27, 2001.
2. Huebner, L. D., Rock, K. E., Ruf, E. G., Witte, D. W., and Andrews, E. H. "Hyper-X Flight Engine Ground Testing for X-43 Flight Risk Reduction," AIAA/NAL-NASDA-ISAS 10th International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto, Japan, AIAA 2001-1809, April 24-27, 2001.
3. Davidson, J., Lallman, F., McMinn, J. D., Martin, J., Pahle, J., Stephenson, M., Selmon, J., and Böse, D., "Flight Control Laws for NASA's Hyper-X Research Vehicle," AIAA Guidance, Navigation, and Control Conference and Exhibit, Portland, OR, AIAA-99-4124, August 9-11, 1999.
4. X-43A Mishap Investigation Board, "Report of Findings X-43A Mishap," NASA, Washington, D.C., Vol. 1, May 8, 2003, also available @www.nasa.gov/pdf747414main_x43A_mishap.pdf.
5. McClinton, C. R., Rausch, V. L., Nguyen, L. T., and Sitz, J. R., "Preliminary X-43 Flight Test Results," IAC 04-V6-X43A 2.
6. Davis, M. C., Pahle, J. W., White, J. T., Marshall, L. A., Mashburn, M. J., and Franks, R., Development of a Flush Airdata Sensing System on a Sharp-Nosed Vehicle for Flight at Mach 3 to 8, NASA-TM-2000-209017, 2000.
7. Bosworth, J. T., and Burken, J. J., Tailored Excitation for Multivariable Stability-Margin Measurement Applied to theX-31A Nonlinear Simulation, NASA TM 113085, 1997.