Conduit—a new multidisciphnary integration environment for flight control development

1997 Guidance, Navigation, and Control Conference

Volumn , Issue , 1997, Pages 1759-1781

  Tischler, Mark B ^a   Colbourne, Jason D ^b   Morel, Mark R ^b   Biezad, Daniel J ^b   Levine, William S ^c   Moldoveanu, Veronica ^c  

^a NASA AMES RESEARCH CENTER   (United States)

^b CALIFORNIA POLYTECHNIC STATE UNIVERSITY   (United States)

^c UNIVERSITY OF MARYLAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEM ANALYSIS; CONTROL SYSTEMS; CONTROL THEORY; DESIGN; ECONOMIC AND SOCIAL EFFECTS; FIXED WINGS; FLIGHT CONTROL SYSTEMS; INTERFACE STATES; MULTIOBJECTIVE OPTIMIZATION; SPECIFICATIONS; SYSTEMS ANALYSIS;

AIRCRAFT FLIGHT CONTROL; DESIGN SPECIFICATION; FLIGHT CONTROL PROBLEMS; FLIGHT TEST PROGRAMS; INTEGRATION ENVIRONMENTS; MULTIOBJECTIVE FUNCTION OPTIMIZATION; SYSTEM ANALYSIS AND DESIGN; SYSTEM SPECIFICATION;

QUALITY CONTROL;

EID: 0042940666     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (22)

1. Tischler, Mark B. (Editor), Advances in Aircraft Flight Control, Taylor and Francis Ltd., Bristol, Pa., 1996.
2. United States Army Aviation Systems Command, “Handling Qualities Requirements for Military Rotorcraft,” ADS-33C, St. Louis, Mo., Aug. 1989.
3. United States Department of Defense, “Flying Qualities of Piloted Vehicles,” MIL-STD-1797, Mar. 1987.
4. Military Specification, Flight Control Systems—General Specifications for Design, Installation, and Test of Piloted Aircraft, MIL-F-9490D, 1975.
5. Tischler, M. B., “System Identification Requirements for High-Bandwidth Rotorcraft Flight Control System Design,” J. Guid., Control, and Dyn., Vol. 13, No. 5, 1990, pp. 835-841.
6. Takahashi, M. D., “Rotor-State Feedback in the Design of Flight Control Laws for a Hovering Helicopter,”J Am. Helicopter Soc., Vol. 39, No. 1, 1994, pp. 52-62.
7. Yudilevitch, G., Tischler, M. B., Levine, W. S., and Lin, C, “Rotorcraft Flight Control System Design Based on Multi-Criterion Parametric Optimization,” AIAA Guidance, Navigation, and Control Conference, Baltimore, Md., Aug. 7-9, 1995.
8. Aiken, E., Jacobsen, R., Eshow, M., Hindson, W., and Doane, D., “Preliminary Design Features of the RASCAL—A NASA/Army Rotorcraft In-Flight Simulator,” AIAA Paper 92-4175, Aug. 1992.
9. Bosworth, John T., “Linearized Aerodynamic and Control Law Models of the X-29A Airplane and Comparison with Flight Data,” NASA TM-4356, 1992.
10. MATLAB®: High-Performance Numeric Computation and Visualization Software. The Math Works, Inc., Reference Guide, 1992.
11. CONSOL-OPTCAD (TM) User's Manual (Version 1.2-1.5, Released May 1992), University of Maryland, College Park, Md., 1992.
12. Tischler, M. B., “System Identification Methods for Aircraft Flight Control Development and Validation,” from Advances in Aircraft Flight Control (Tischler, M. B., Editor), Taylor and Francis Ltd., Bristol, Pa., 1996.
13. Mitchell, David G. and Hoh, Roger H., “Proposed Incorporation of Mission-Oriented Flying Qualities into MIL-STD 1797A,” WL-TR-94-3162, Oct. 1994.
14. Panier, E. R. and Tits, A. L. “On Combining Feasibility, Descent, and Superlinear Convergence in Equality Constrained Optimization,” Math. Programming, Vol. 59, 1993, pp. 261-276.
15. Lawrence, C., Zhou, J. L., and Tits, A. L., “User's Guide for CFSQP Version 2.4: A C Code for Solving (Large Scale) Constrained Nonlinear (Minimax) Optimization Problems, Generating Iterates Satisfying All Inequality Constraints,” University of Maryland, College Park, Md., 1996.
16. Glusman, S. L, Dabundo, C., and Landis, K. H., “Evaluation of ADOCS Demonstrator Handling Qualities,” Proceedings of the 43rd Annual National Forum of the American Helicopter Society, Washington, D.C., May 1987.
17. Catapang, D. R., Tischler, M. B., and Biezad, D. J., “Robust Crossfeed Design for Hovering Rotorcraft,” Int'l. J. Robust and Nonlinear Control, Vol. 4, No. 1, Jan.-Feb. 1994.
18. Fletcher, J. W., “Identification of UH-60 Stability Derivative Models in Hover from Flight Test Data,” J. Am. Helicopter Soc., Vol. 40, No. 1, 1995, pp. 32-46.
19. Tischler, M. B., Fletcher, J. W., Patrick, P. M., Morris, M., and Tucker, G. E., “Flying Quality Analysis and Flight Evaluation of a Highly Augmented Combat Rotorcraft,” J. Guid., Control, and Dyn., Vol. 14, No. 5, 1991, pp. 954-963.
20. Clarke, Robert, Burken, John J., Bosworth, John T., and Bauer, Jeffrey E., “X-29 Flight Control System: Lessons Learned,” from Advances in Aircraft Flight Control (Tischler, M. B., Editor), Taylor and Francis Ltd., Bristol, Pa., 1996.
21. Bosworth, John T. and Cox, Timothy H., “A Design Procedure for the Handling Qualities Optimization of the X-29A Aircraft,” NASA TM-4142, 1989.
22. Neal, T. P. and Smith, R. E., “An In-Flight Investigation to Develop Control System Design Criteria for Fighter Airplanes, Volume I,” AFFDL-TR-70-74, Dec. 1970.