Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Highly Integrated Digital Electronic Control: Digital Flight Control, Aircraft Model Identification, and Adaptive Engine Control
Performance Improvements of a Highly Integrated Digital Electronic Control System for an F-15 Airplane
Predicted Performance Benefits of an Adaptive Digital Engine Control System of an F-15 Airplane
Highly Integrated Digital Engine Control System on an F-15 Airplane
An Electronic Workshop on the Performance Seeking Control and Propulsion Controlled Aircraft Results of the F-15 Highly Integrated Digital Electronic Control Flight Research Program
Propulsion Control Experience Used in the Highly Integrated Digital Electronic Control (HIDEC) Program
Propulsion System-flight Control Integration and Optimization: Flight Evaluation and Technology Transition
NASA Technical Memorandum
Digital Adaptive Flight Controller Development
Author: Howard Kaufman
Publisher:
ISBN:
Category : Adaptive control systems
Languages : en
Pages : 132
Book Description
A design study of adaptive control logic suitable for implementation in modern airborne digital flight computers was conducted. Two designs are described for an example aircraft. Each of these designs uses a weighted least squares procedure to identify parameters defining the dynamics of the aircraft. The two designs differ in the way in which control law parameters are determined. One uses the solution of an optimal linear regulator problem to determine these parameters while the other uses a procedure called single stage optimization. Extensive simulation results and analysis leading to the designs are presented.
Publisher:
ISBN:
Category : Adaptive control systems
Languages : en
Pages : 132
Book Description
A design study of adaptive control logic suitable for implementation in modern airborne digital flight computers was conducted. Two designs are described for an example aircraft. Each of these designs uses a weighted least squares procedure to identify parameters defining the dynamics of the aircraft. The two designs differ in the way in which control law parameters are determined. One uses the solution of an optimal linear regulator problem to determine these parameters while the other uses a procedure called single stage optimization. Extensive simulation results and analysis leading to the designs are presented.
Research in Digital Adaptive Flight Controllers
Author: Howard Kaufman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 106
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 106
Book Description