摘要
提出了一种三自由度模型姿态调整机构。采用回转矩阵方法分析了模型姿态与输入角度的关系,给出了机构的正解,结果表明模型姿态的三个自由度之间存在耦合关系,且表现出非线性。利用机构的运动特点,采用几何方法给出了反解,避免了数值解法的缺陷。
A three degree-of-freedom attitude adjustment mechanism is proposed. Direct kinematics was studied and the results indicate that the relationship between the angles the supporting system rotates and the attitude (α,β,γ)of the model is nonlinear and coupled. Based on the specific structure of the supporting system, geometric method was adopted to obtain the inverse solution.
出处
《国防科技大学学报》
EI
CAS
CSCD
北大核心
2004年第2期84-88,共5页
Journal of National University of Defense Technology
基金
国家自然科学基金-香港青年学者合作研究基金资助项目(50029501)
关键词
姿态调整机构
模型支撑系统
运动学分析
attitude-adjusting system
model supporting system
kinematics analysis
