Desired trajectory and guidance force generators for an aircraft

1996 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1996, Pages 1-9

  Baba, Yoriaki ^a,b   Takano, Hiroyuki ^a,b   Sano, Masaki ^a,b  

^a NATIONAL DEFENSE ACADEMY   (Japan)

^b NDA   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRCRAFT CONTROL; COMPUTER CIRCUITS; CONTROLLERS; ERROR CORRECTION; FLIGHT CONTROL SYSTEMS; FUZZY LOGIC; INTERPOLATION; TRAJECTORIES;

AIRCRAFT GUIDANCE; AUTOMATIC FLIGHT; CUBIC SPLINE FUNCTIONS; DESIRED TRAJECTORIES; INDEPENDENT VARIABLES; INTERCEPT POINTS; MINIMUM CURVATURE; TRAJECTORY GENERATOR;

AIR NAVIGATION;

EID: 84959114944     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-3873     Document Type: Conference Paper

References (11)

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8. Snell, S. A., Enns, D. F. and Garrard W. Jr.,”Nonlinear Invertion Flight Control for a Supermaneuverable Aircraft”, AIAA-90-3406-CP, 1990,pp.808-825.
9. Ahlberg, J.H., Nilson E. N. and Walsh, J. L, “The Theory of Splines and Their Applications”, Academic Press (1967)
10. Lee, C. C.,”Fuzzy Logic in Control Systems: Fuzzy Logic Controller, Parts 1,2”, IEEE Transactions Systems, Man, Cybernetics, Vol.20, March/April 1990, pp.404-439.
11. Eulrich, B. J. and Weingarten, N.C., “Identification and Correlation on the F-4E Stall/Poststall Aerodynamic Stability and Control Characteristics from Existing Test Data, National Technical Information Service, U.S. Department of Commerce, AD-779-928(1973).