Determination of X-36 stability margins using real-time frequency response techniques

23rd Atmospheric Flight Mechanics Conference

Volumn , Issue , 1998, Pages 105-115

  Balough, Dwight L ^a  

^a NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MANUFACTURE; CONTROL THEORY; FLIGHT CONTROL SYSTEMS; FLIGHT ENVELOPES; FLIGHT SIMULATORS; FREQUENCY ESTIMATION; FREQUENCY RESPONSE; NASA; SOFTWARE TESTING; STABILITY; TRACTION (FRICTION); TRANSFER FUNCTIONS;

FIGHTER CONFIGURATION; FREQUENCY RESPONSE TECHNIQUE; MEASUREMENT TECHNIQUES; OPEN-LOOP TRANSFER FUNCTIONS; REAL-TIME APPLICATION; REMOTELY PILOTED AIRCRAFT; SINGLE INPUT , SINGLE OUTPUTS; SINGULAR-VALUE ANALYSIS;

RESEARCH AIRCRAFT;

EID: 84983185773     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-4154     Document Type: Conference Paper

References (10)

1. Bosworth, J. T., "Flight-Determined Longitudinal Stability Characteristics of the X-29A Airplane Using Frequency Response Techniques," NASA TM 4122, June 1989.
2. Clarke, R., Burken, J. J., Bosworth, J. T., Bauer, J. E., "X-29 Flight Control System: Lessons Learned," AGARD/NATO Flight Mechanics Panel Symposium, Turin, Italy, May 1994.
3. Tischler, M. B., Cauffman, M. G., "Comprehensive Identification from FrEquency Responses, Volume 2-User's Manual," NASA CP 10150, Sept. 1994.
4. Anon, MATRIX. ™ Core Manual. Edition 8. Integrated Systems, Inc. Santa Clara, CA, 1991.
5. Bendat, J. S., Piersol, A. G., Random Data: Analysis and Measurement Procedures. Wiley and Sons, New York, NY, 1986, pp 361-424.
6. Anon, MATLAB™ Hiph-Performance Numeric Computation and Visualization Software Reference Guide. The MathWorks, Inc., Natick, MA, 1994.
7. Harris, W. J., "X-36 Tailless Agility Aircraft Subystems Integration," Society of Automotive Engineers, Inc. Paper 97-WAC-18, August 1997.
8. Ly, U. L., "Robustness Analysis of a Multiloop Flight Control System," AIAA Paper 83-2189, August 1983.
9. Mukhopadhyay, V., Newsom, J. R., "A Multiloop System Stability Margin Study Using Matrix Singular Values," AIAA Paper 82-1574, San Diego, CA, August 1982.
10. Burken, J. J., "Flight-Determined Stability Analysis of Multiple-Input-Multiple-Output Control Systems," NASA TM 4416, Nov. 1992.