Advances in aircraft flight control.
Advances in aircraft flight control.
, edited by Mark B. Tischler
- London Taylor c. 1996
- xvii, 423 p. il. byn, cuadros, gráficos
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.
0748404791
AVIONES
CONTROL DE VUELO
TECNOLOGIA AERONAÚTICA
629.73.05=111 ADV
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.
0748404791
AVIONES
CONTROL DE VUELO
TECNOLOGIA AERONAÚTICA
629.73.05=111 ADV