Quaternion Method for Kinematics Modeling of High Attack-Angle Flying Carrier
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Quaternion Method for Kinematics Modeling of High Attack-Angle Flying Carrier
大攻角飞行载体运动学建模的四元数方法研究
Issue 3, Pages: 276-279(2006)
作者机构:
中北大学电子测试技术国家重点实验室
作者简介:
基金信息:
DOI:
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Published:2006
稿件说明:
移动端阅览
秦丽, 张文栋, 潘峰. Quaternion Method for Kinematics Modeling of High Attack-Angle Flying Carrier[J]. 2006, (3): 276-279.
DOI:
秦丽, 张文栋, 潘峰. Quaternion Method for Kinematics Modeling of High Attack-Angle Flying Carrier[J]. 2006, (3): 276-279.DOI:
Quaternion Method for Kinematics Modeling of High Attack-Angle Flying Carrier
摘要
针对大攻角飞行载体运动特征
在比较传统飞行力学中描述小攻角飞行载体姿态常用的几种方法的基础上
提出大攻角飞行载体运动学建模的四元数方法
将此四元数方法应用于飞行载体姿态解算方法中进行了仿真计算和分析
仿真结果表明
大攻角飞行载体运动学建模的四元数方法对飞行载体在飞行过程中的姿态描述是有效和适用的.
Abstract
Based on the comparison of several methods in conventional flight mechanics for characterizing the kinematics of flying carrier at low angles of attack
this paper has presented a quaternion method for kinematics modeling of high attack-angle flying carriers in accordance with the motion characters of high attack-angle flying carriers.Simulation of and analysis on the quaternion method prove that the quaternion method for kinematics modeling of high attack-angle flying carrier is suitable for effective characterization of the flying carrier′s motion during flight.
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references
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