Automatic Flight Control Systems

Introduction to Tool-Based Design and Evaluation of Resilient Flight Control Systems

A large transport aircraft simulation benchmark (REconfigurable COntrol for Vehicle Emergency Return RECOVER) has been developed within the European GARTEUR Flight Mechanics Action  Group 16  (FM-AG(16))  on  Fault  Tolerant Control (2004-2008)  for  the integrated evaluation of fault detection, identification (FDI) and  reconfigurable flight control systems. The  benchmark includes a  suitable set  of  assessment criteria  and  failure  cases, based on reconstructed accident scenarios, to assess the potential of new adaptive control strategies to improve aircraft survivability. The application of reconstruction and modeling techniques, using accident flight data for validation, has resulted in high fidelity non-linear…

Boomi Nathan

Introduction to Quantitative Feedback Theory and Its Application in UAV’s Flight Control

Quantitative feedback theory (hereafter referred as QFT), developed by Isaac Horowitz (Horowitz, 1963; Horowitz and Sidi, 1972), is a frequency domain technique utilizing the Nichols chart in order to achieve a desired robust design over a specified region of plant uncertainty.  Desired  time-domain  responses  are  transformed  into  frequency  domain tolerances, which  lead  to  bounds (or  constraints) on  the  loop  transmission function. The design  process  is  highly  transparent,  allowing  a  designer  to  see  what  trade-offs  are necessary to achieve  a desired performance level. QFT is also a unified theory that  emphasizes the use  of feedback for achieving the desired system performance tolerances despite plant uncertainty and plant disturbances.…

Boomi Nathan

Introduction to Gain Tuning of Flight Control Laws for Satisfying Trajectory Tracking Requirements

The present chapter is concerned with presenting an approach for the synthesis of a gain- scheduled flight  control  law  that  assures compliance to  trajectory tracking requirements. More precisely, a strategy is proposed for improving the tracking performances of a baseline controller, obtained by conventional synthesis techniques, by tuning its gains.  The approach is specifically designed for atmospheric re-entry applications, in which  gain scheduled flight control  laws are typically used. Gain-scheduling design approaches conventionally construct a nonlinear controller by combining the members of an appropriate family of linear time-invariant (LTI) controllers…

Boomi Nathan
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