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Advances in aircraft flight control. , edited by Mark B. Tischler

Colaborador(es): Tipo de material: Archivo de ordenadorArchivo de ordenadorDetalles de publicación: London Taylor c. 1996Descripción: xvii, 423 p. il. byn, cuadros, gráficosISBN:
  • 0748404791
Tema(s):
Contenidos:
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.
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Libro Libro Biblioteca Dr. Jorge S. Muntaner Coll 629.73.05=111 ADV (Navegar estantería(Abre debajo)) Disponible 005970

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.

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