Constructing & Simulating a Mathematical Model of
2016-08-23
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This paper will present detailed procedure of how to construct a basic mathematical model
that represents general longitudinal helicopter flight dynamics. The procedure will start from
linearizing the translational and rotational dynamics and rotational kinematics equations of
motion using the small perturbation theory. There are certain assumptions made for the sake
of simplifications. The next step is to construct the fundamental linearized form for describing
the stability and response of a small motion of a helicopter around a trim condition. In order to
simulate the results, basic input data from an existing helicopter will be used. The last step is
that represents general longitudinal helicopter flight dynamics. The procedure will start from
linearizing the translational and rotational dynamics and rotational kinematics equations of
motion using the small perturbation theory. There are certain assumptions made for the sake
of simplifications. The next step is to construct the fundamental linearized form for describing
the stability and response of a small motion of a helicopter around a trim condition. In order to
simulate the results, basic input data from an existing helicopter will be used. The last step is
matlab
模型
模拟
直升机
动力学
飞行
数学
构建
纵向
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