TY - DATA AU - Tischler, Mark B. TI - Advances in aircraft flight control SN - 0748404791 PY - 1996/// CY - London PB - Taylor KW - AVIONES KW - CONTROL DE VUELO KW - TECNOLOGIA AERONAÚTICA N1 - Colección de artículos organizados en cuatro partes: 1)Specification and validation methods ; 2) Rotorcraft and V/STOL; 3) Transport aircraft; 4) High-performance aircraft; Indice alfabético, al final del libro; Referencias bibliográficas, al final de cada artículo. ; Handling-qualities specification : a functional requierement for the flight control system /; R. H. Hoh and D. G. Mitchell; System identification methods for aircraft flight control development and validation /; M. B. Tischler; A high bandwidth control system for the helicopter in-flight simulator ATTHeS : modelling, performance and applications /; W. von Grünhagen, G. Bouwer, H. -J. Pausder, F. Henschel and J. Kaletka; Advanced flight control research and development at Boeing helicopters /; K. H. Landis, J. M. Davis, C. Dabundo and J. F. Keller; Application of nonlinear inverse methods to the control of powered-lift aircraft over the low-speed flight envelope /; J. A. Franklin; Flight control and handling research withthe VAAC Harrier aircraft /; G. T. Shanks, S. L. Gale, C. Fielding and D. V. Griffith; The design and development of flying qualities for the C-17 military transport airplane /; E. R. Kendall; Fly-by-wire for commercial aircraft : the Airbus experience /; C. Favre; Practical control law design for aircraft using multivariable techniques /; J. D. Blight, R. L. Dailey and D. Gangsaas; Lavi flight control system /; M. Shmul, E. Erenthal and M. Attar; Digital autopilot design for combat aircraft in Alenia /; A. Tonon and P. L. Belluati; Development and flight experience of the control laws and the aeroservoelastic solution in the Experimental Aircraft Programme (EAP) /; A. McCuish and B. Caldwell; X-29 flight control system : lessons learned /; R. Clarke, J. J. Burken, J. T. Bosworth and J. E. Bauer; Practical aspects of the design of an integrated flight and propulsion control system /; D. J. Moorhouse and K. D. Citurs; Control law design and flight test results of the experimental aircraft X-31A /; H. Beh,G. Hofinger and P. Huber ER -