Adaptive Flight Control to Enhance Survivability and Reduce Cost of Change

Lead Research Organisation: Cranfield University
Department Name: Sch of Aerospace, Transport & Manufact

Abstract

A number of applications of AI learning to control system design have been reported. These studies have been focusing on the controller design for the systems that have relatively simple dynamic characteristics such as car, robot manipulator, or pendulum. However, it is well-known that the dynamics characteristics of aircraft or UAS are relatively complicated: high nonlinear, rapidly changing dynamics, and uncertainties of aerodynamic parameters. Thus, the fundamental research question of this PhD programme is how to select an appropriate architecture of AI learning in order to find feasible and safe solution for such a complicated system. Another challenge is the validation of solution. The autopilot based on AI learning is generally considered as a "block-box" approach. The main problem of such a kind of approach is that no one can guarantee whether or not it will not make any issues when implementing it in a real system. However, previous studies have mostly focused on showing the feasibility only, but there has been lack of effort to validate such a block-box approach. Namely, understandings of the behaviour of black-box and the convergence of solution have been less understood. In practice, these are important in ensuring confidence in the performance and reliability of learning-based approach when implementing the autopilot based on learning-based approach in a real system.This research seeks an appropriate AI learning architecture for controlling of complicated dynamics systems such as aircraft or UAS. The innovation proposed will investigate a way to understand the behaviour of autopilot based on learning approach. The principle contribution will be a practical autopilot algorithm based on learning approach which is directly applicable to real systems in ensuring confidence in the reliability. The scientific value and innovation thus lie in not only development of a novel and a practical and reusable autopilot algorithm for aircraft or UAS, but also validation of the proposed algorithm based on theoretical analyses, numerical simulation, and flight tests. The primary aim of this project is to develop a practical and safe autopilot algorithm based on AI learning approach that can easily reconfigure its control algorithm according to the model changes. The overall approach is a combination of theoretical innovation with numerical simulations or flight test. Therefore, the specific objectives will include: a. Review state-of-the-art learning approaches and investigate their applicability to the flight control system; b. Develop realistic flight models; c. Develop a flight control system based on the most promising state-of-art AI learning approaches; d. Investigate an appropriate architecture of the adaptive flight control system developed; e. Identify relevant performance metrics for the adaptive flight control system; f. Investigate appropriate methods for the validation and verification of adaptive flight control systems; g. Analyse and validate the designed flight control system using the flight test-bed and performance metrics developed.

Publications

10 25 50

Studentship Projects

Project Reference Relationship Related To Start End Student Name
EP/S513623/1 01/10/2018 30/09/2024
2278904 Studentship EP/S513623/1 01/10/2019 30/03/2023 Matthew Osborne
 
Description An extensive review of safe learning techniques for nonlinear control systems.
A bridging of the gap between nonlinear control techniques using contraction metrics and convex optimisation and traditional linear time invariant controller design using pole placement or linear control theory.
A novel algorithm that generates a control policy using this new knowledge to optimise a contraction metric for flying qualities specifications.
The first application of control contraction metrics for a military aircraft flight controller.
Limitations or complexities around the implementation of nonlinear control techniques using control contraction metrics for flight controllers.
Exploitation Route Further optimisation and application of the techniques developed for higher dimensions and for a greater number of applications is possible in many other science and engineering fields.
The work provides a good benchmark and reference material to expand upon.
Sectors Aerospace, Defence and Marine,Education,Other

URL https://ieeexplore.ieee.org/document/9476765