2018 Atmospheric Flight Mechanics Conference 2018
DOI: 10.2514/6.2018-3312
|View full text |Cite
|
Sign up to set email alerts
|

A Learn-to-Fly Approach for Adaptively Tuning Flight Control Systems

Abstract: A method is presented for adaptively tuning feedback control gains in a flight control system to achieve desired closed-loop performance. The method combines efficient parameter estimation for identifying closed-loop dynamics models, with online nonlinear optimization for sequentially perturbing and updating control gains to improve performance. Prior information on stability and control derivatives is not needed, nor is any knowledge about the control system architecture. Following convergence, the optimized … Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2

Citation Types

0
2
0

Year Published

2018
2018
2024
2024

Publication Types

Select...
3
3

Relationship

0
6

Authors

Journals

citations
Cited by 10 publications
(2 citation statements)
references
References 21 publications
0
2
0
Order By: Relevance
“…The advantages of L2F include the use of aerodynamic models based on real-time identification of flight data in the control law design. Therefore, there is no need to modify the Reynolds number, blockage, boundary layer turbulence, etc [15][16][17]. The control system design is developed based on the actual flight dynamics response rather than the simulation results.…”
Section: Introductionmentioning
confidence: 99%
“…The advantages of L2F include the use of aerodynamic models based on real-time identification of flight data in the control law design. Therefore, there is no need to modify the Reynolds number, blockage, boundary layer turbulence, etc [15][16][17]. The control system design is developed based on the actual flight dynamics response rather than the simulation results.…”
Section: Introductionmentioning
confidence: 99%
“…The work presented here is part of a feasibility study of the Learn-to-Fly concept. While other modeling and control techniques could also be employed [4,5], this paper examines two approaches to the Learn-to-Fly online control design problem. One approach is based on a nonlinear dynamic inversion method with the addition of an adaptive disturbance rejection module.…”
Section: Introductionmentioning
confidence: 99%