Singular Perturbations and Time Scales in the Design of Digital Flight Control Systems 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 Singular Perturbations and Time Scales in the Design of Digital Flight Control Systems PDF full book. Access full book title Singular Perturbations and Time Scales in the Design of Digital Flight Control Systems by Desineni S. Naidu. Download full books in PDF and EPUB format.

Singular Perturbations and Time Scales in the Design of Digital Flight Control Systems

Singular Perturbations and Time Scales in the Design of Digital Flight Control Systems PDF Author: Desineni S. Naidu
Publisher:
ISBN:
Category : Control theory
Languages : en
Pages : 36

Book Description


Singular Perturbations and Time Scales in the Design of Digital Flight Control Systems

Singular Perturbations and Time Scales in the Design of Digital Flight Control Systems PDF Author: Desineni S. Naidu
Publisher:
ISBN:
Category : Control theory
Languages : en
Pages : 36

Book Description


Singular Perturbations and Time Scales in the Design of Digital Flight Control Systems

Singular Perturbations and Time Scales in the Design of Digital Flight Control Systems PDF Author: Desineni S. Naidu
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

Book Description


Singular Perturbations and Time Scales in the Design of Digital Flight Control Systems

Singular Perturbations and Time Scales in the Design of Digital Flight Control Systems PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722771010
Category :
Languages : en
Pages : 34

Book Description
The results are presented of application of the methodology of Singular Perturbations and Time Scales (SPATS) to the control of digital flight systems. A block diagonalization method is described to decouple a full order, two time (slow and fast) scale, discrete control system into reduced order slow and fast subsystems. Basic properties and numerical aspects of the method are discussed. A composite, closed-loop, suboptimal control system is constructed as the sum of the slow and fast optimal feedback controls. The application of this technique to an aircraft model shows close agreement between the exact solutions and the decoupled (or composite) solutions. The main advantage of the method is the considerable reduction in the overall computational requirements for the evaluation of optimal guidance and control laws. The significance of the results is that it can be used for real time, onboard simulation. A brief survey is also presented of digital flight systems. Naidu, Desineni S. and Price, Douglas B. Langley Research Center RTOP 506-46-21-01...

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 978

Book Description


NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 172

Book Description


NASA Scientific and Technical Publications

NASA Scientific and Technical Publications PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 64

Book Description


Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1586

Book Description


Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1224

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1148

Book Description


Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1986

Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1986 PDF Author: Langley Research Center. Research Information and Applications Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 270

Book Description