Linearized Aerodynamic and Control Law Models of the X-29A Airplane and Comparison with Flight Data PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Linearized Aerodynamic and Control Law Models of the X-29A Airplane and Comparison with Flight Data PDF full book. Access full book title Linearized Aerodynamic and Control Law Models of the X-29A Airplane and Comparison with Flight Data by John T. Bosworth. Download full books in PDF and EPUB format.
Author: John T. Bosworth
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 120
Get Book Here
Book Description
Author: John T. Bosworth
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 120
Get Book Here
Book Description
Author: John T. Bosworth
Publisher:
ISBN:
Category :
Languages : en
Pages : 120
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 120
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 320
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
Get Book Here
Book Description
A state-of-the-art computational facility for aircraft flight control design, evaluation, and integration called CONDUIT (Control Designer's Unified Interface) has been developed. This paper describes the CONDUIT tool and case study applications to complex rotary- and fixed- wing fly-by-wire flight control problems. Control system analysis and design optimization methods are presented, including definition of design specifications and system models within CONDUIT, and the multi-objective function optimization (CONSOL-OPTCAD) used to tune the selected design parameters. Design examples are based on flight test programs for which extensive data are available for validation. CONDUIT is used to analyze baseline control laws against pertinent military handling qualities and control system specifications. In both case studies, CONDUIT successfully exploits trade-offs between forward loop and feedback dynamics to significantly improve the expected handling qualities and minimize the required actuator authority. The CONDUIT system provides a new environment for integrated control system analysis and design, and has potential for significantly reducing the time and cost of control system flight test optimization.
Author: Brent R. Cobleigh
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 40
Get Book Here
Book Description
Author: Hua Harry Li
Publisher: Springer Science & Business Media
ISBN: 0585280002
Category : Mathematics
Languages : en
Pages : 455
Get Book Here
Book Description
One of the attractions of fuzzy logic is its utility in solving many real engineering problems. As many have realised, the major obstacles in building a real intelligent machine involve dealing with random disturbances, processing large amounts of imprecise data, interacting with a dynamically changing environment, and coping with uncertainty. Neural-fuzzy techniques help one to solve many of these problems. Fuzzy Logic and Intelligent Systems reflects the most recent developments in neural networks and fuzzy logic, and their application in intelligent systems. In addition, the balance between theoretical work and applications makes the book suitable for both researchers and engineers, as well as for graduate students.
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 846
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1388
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
Get Book Here
Book Description
