A bank angle protection method based on potential functions for nonlinear aircraft model

Donglei Sun, Naira Hovakimyan

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

This paper presents a bank angle protection method for a nonlinear aircraft model. In previous study, a bank angle protection strategy was proposed based on the potential function method and tested on the linearized NASA Transport Class Model. In this paper, the potential function is modified for an improved damping performance. A switched envelope protection law is then proposed for pilot command of different magnitude to reduce the region where the envelope protection takes effect. Exponential stability of the closed-loop system with this new design is proved under some mild conditions to justify its validity. Simulation examples of bank angle protection design for NASA's nonlinear Transport Class Model are provided to verify the efficacy of the proposed design.

Original languageEnglish (US)
Title of host publication17th AIAA Aviation Technology, Integration, and Operations Conference, 2017
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624105081
StatePublished - Jan 1 2017
Event17th AIAA Aviation Technology, Integration, and Operations Conference, 2017 - Denver, United States
Duration: Jun 5 2017Jun 9 2017

Publication series

Name17th AIAA Aviation Technology, Integration, and Operations Conference, 2017

Other

Other17th AIAA Aviation Technology, Integration, and Operations Conference, 2017
CountryUnited States
CityDenver
Period6/5/176/9/17

Fingerprint

Aircraft models
NASA
Asymptotic stability
Closed loop systems
Damping

ASJC Scopus subject areas

  • Aerospace Engineering
  • Energy(all)

Cite this

Sun, D., & Hovakimyan, N. (2017). A bank angle protection method based on potential functions for nonlinear aircraft model. In 17th AIAA Aviation Technology, Integration, and Operations Conference, 2017 (17th AIAA Aviation Technology, Integration, and Operations Conference, 2017). American Institute of Aeronautics and Astronautics Inc, AIAA.

A bank angle protection method based on potential functions for nonlinear aircraft model. / Sun, Donglei; Hovakimyan, Naira.

17th AIAA Aviation Technology, Integration, and Operations Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, 2017. (17th AIAA Aviation Technology, Integration, and Operations Conference, 2017).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Sun, D & Hovakimyan, N 2017, A bank angle protection method based on potential functions for nonlinear aircraft model. in 17th AIAA Aviation Technology, Integration, and Operations Conference, 2017. 17th AIAA Aviation Technology, Integration, and Operations Conference, 2017, American Institute of Aeronautics and Astronautics Inc, AIAA, 17th AIAA Aviation Technology, Integration, and Operations Conference, 2017, Denver, United States, 6/5/17.
Sun D, Hovakimyan N. A bank angle protection method based on potential functions for nonlinear aircraft model. In 17th AIAA Aviation Technology, Integration, and Operations Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA. 2017. (17th AIAA Aviation Technology, Integration, and Operations Conference, 2017).
Sun, Donglei ; Hovakimyan, Naira. / A bank angle protection method based on potential functions for nonlinear aircraft model. 17th AIAA Aviation Technology, Integration, and Operations Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, 2017. (17th AIAA Aviation Technology, Integration, and Operations Conference, 2017).
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