Generalized Dynamic Inversion Based Aircraft LateraL Control

Authors

  • Alharith Mahmoud King Abdulaziz University, Aeronautical Engineering Department,Jeddah,21589
  • Abdulrahman H. Bajodah King Abdulaziz University, Aeronautical Engineering Department,Jeddah,21589

Keywords:

Null control vector, Projection matrix, Generalized dynamic inversion, Lateral control, Virtual constraint dynamics

Abstract

This paper illustrates how the Generalized Dynamic inversion (GDI) is used to control aircraft lateral motion. To implement the GDI control law, the yaw channel constraint dynamics are first constructed and then inverted using Moore-Penrose Generalized Inverse (MPGI). Consequently, the auxiliary component of this control law is affine in a null control vector, which is designed to guarantee asymptotic aircraft stability. Asignificant benefit of GDI  control law is the additional design flexibility afforded by its two independent control actions. Extensive simulations have been conducted to prove the efficacy of the proposed method.

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Published

2022-12-04

How to Cite

Alharith Mahmoud, & Abdulrahman H. Bajodah. (2022). Generalized Dynamic Inversion Based Aircraft LateraL Control. International Journal of Sciences: Basic and Applied Research (IJSBAR), 65(1), 238–247. Retrieved from https://gssrr.org/index.php/JournalOfBasicAndApplied/article/view/14953

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