Design of aircraft lateral control laws simulation for teaching and learning
This paper studies the design of a simulator to simulate the general behaviour of an aircraft in its lateral motion. The study will be in two parts: the aircraft lateral natural system and the design of the control laws. In the aircraft lateral natural system, all modes will be discussed including...
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| 主要な著者: | , , , , |
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| フォーマット: | 論文 |
| 言語: | English |
| 出版事項: |
Penerbit Universiti Kebangsaan Malaysia
2021
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| オンライン･アクセス: | http://journalarticle.ukm.my/19073/1/15.pdf http://journalarticle.ukm.my/19073/ https://www.ukm.my/jkukm/si-41-2021/ |
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| 要約: | This paper studies the design of a simulator to simulate the general behaviour of an aircraft in its lateral motion. The
study will be in two parts: the aircraft lateral natural system and the design of the control laws. In the aircraft lateral
natural system, all modes will be discussed including the Pure Roll mode, the Dutch Roll mode, and the Spiral mode. In
the design of the control laws, two types of control laws were discussed which are the yaw damper and the poles
placement method. The result is a complete simulator for aircraft lateral motion which allows the user to simulate and
study the lateral characteristic of an aircraft given the desired input. The simulator resulted from this study is suitable
to be used for teaching and learning as the changes in parameters yield instantaneous results that can be displayed. |
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