Modeling and Motion Analysis of Fixed-Pitch Co-Axial Rotor Unmanned Helicopter

机译：固定间距共轴转子无人直升机的建模与运动分析

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In this study, dynamics of a fixed-pitch co-axial rotor unmanned helicopter is modeled, and fundamental motion analysis is performed using derived model. The unmanned helicopter is considered as a rigid body system consists of 2 rigid bodies, and multi-body dynamics modeling technique named velocity transformation method is used for deriving the equation of motion. Force and torque terms applied to the helicopter are obtained by using aerodynamics of co-axial rotors including aerodynamic interference between upper and lower rotor. Finally, the motion analysis using the model is performed to establish the relation between the motion and the mechanical specification of fixed-pitch co-axial rotor unmanned helicopter.

机译：在该研究中，建模固定桨距协调转子无人直升机的动力学，并且使用衍生模型进行基本运动分析。无人驾驶直升机被认为是刚体系统，由2个刚体组成，并且使用的多体动力学建模技术命名为Velocity变换方法，用于导出运动方程。通过使用共轴转子的空气动力学来获得施加到直升机的力和扭矩术语，包括上部和下转子之间的空气动力学干涉。最后，执行使用该模型的运动分析来建立运动与固定间距共轨无人直升机的运动和机械规格之间的关系。

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《IEEE/RSJ International Conference on Intelligent Robotics and Systems》|2012年||共6页
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Suzuki Satoshi; Ishii Takahiro; Yanagisawa Gennai; Tomita Kazuki; Yokoyama Yasutoshi;
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中图分类 TP242.6-53;
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2. Modelling and robust control of an unmanned coaxial rotor helicopter with unstructured uncertainties: [J] . Zhi-Yan Dong, Shun-An Liu, Chao Liu, Advances in Mechanical Engineering . 2017,第1期

机译：具有非结构化不确定性的无人同轴旋翼直升机的建模和鲁棒控制：
3. Modelling and robust control of an unmanned coaxial rotor helicopter with unstructured uncertainties: [J] . Zhi-Yan Dong, Shun-An Liu, Chao Liu, Advances in Mechanical Engineering . 2017,第1期

机译：具有非结构化不确定性的无人同轴旋翼直升机的建模和鲁棒控制：
4. Modeling and motion analysis of fixed-pitch co-axial rotor unmanned helicopter [C] . Suzuki Satoshi, Ishii Takahiro, Yanagisawa Gennai, IEEE/RSJ International Conference on Intelligent Robots and Systems;IROS 2012 . 2012

机译：固定螺距同轴转子无人直升机的建模与运动分析
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Modeling and Motion Analysis of Fixed-Pitch Co-Axial Rotor Unmanned Helicopter

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