Aircraft Longitudinal Control based on the Lanchester's Phugoid Dynamics Model

被引：0

作者：

Rosario-Gabriel, I. ^{[1
]}

Rodriguez Cortes, H. ^{[1
]}

机构：

[1] Inst Politecn Nacl, Ctr Invest & Estudios Avanzados, Av Inst Politecn Nacl 2508, Ciudad De Mexico 07360, Mexico

来源：

2018 INTERNATIONAL CONFERENCE ON UNMANNED AIRCRAFT SYSTEMS (ICUAS) | 2018年

关键词：

CONTROLLED LAGRANGIANS; STABILIZATION; STABILITY; VEHICLES; LIFT;

D O I：

暂无

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

This paper presents a longitudinal aircraft controller inspired by the polar equation of the hodograph, one of the invariants of the Lanchester's phugoid dynamics. The control design procedure follows the considerations made by Lancaster to develop the Phugoid dynamics, this is, the angle of attack is quasi-static. Then, it is possible to design a longitudinal aircraft dynamics controller that requires knowing the elevator control derivative coefficient, and the aircraft physical characteristics. The control design procedure assumes a known structure for the aircraft aerodynamic characteristics. Closed-loop stability properties rely on considering that the angle of attack is small and boundedness of the lift coefficient. Numerical simulations using the X-Plane flight simulator validate the proposed controller.

引用

页码：924 / 929

页数：6

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