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1Cubic polynomial trajectory planning algorithm Based on ideal drive force for Aircraft fusagle Automatic Position and Pose Adjustment

机译:基于机摩苏自动位置理想驱动力的基于理想驱动力和姿态调整的1个Cubic多项式轨迹规划算法

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In order to ensure the stationarity of the aircraft fusagle automatic adjustment and reduce the fluctuation of the drive force, the redundant actuation optimal algorithm is presented in this paper. Firstly, using Newton-Euler method, the dynamics equations of pose adjustment system are established. Based on the equations, the driving forces can be sovled. Secondly, according to the constraint conditions and pose adjustement process, Cubic Polynomial trajectory planning algorithm is proposed for the aircraft fusagle automatic adjustment. Thirdly, in order to reduce the fluctuation of the drive force, the redundant actuation optimal algorithm is presented. Simulation results show that the presented trajectory planning algorithm has good dynamic characteristics and satisfies engineering requirements. Moreover, the differences between the solutions of optimal algorithm and ideal drive forces are much less than the differences between the minimal norm least square solution and ideal drive forces.
机译:为了确保飞机熔丝自动调节和降低驱动力的波动,本文介绍了冗余致动最佳算法。首先,使用牛顿 - 欧拉方法,建立了姿势调整系统的动态方程。基于方程式,可以围绕驱动力。其次,根据约束条件和姿势调节过程,提出了对飞机摩苏尔自动调整的立方多项式轨迹规划算法。第三,为了降低驱动力的波动,提出了冗余致动最佳算法。仿真结果表明,所呈现的轨迹规划算法具有良好的动态特性,满足工程要求。此外,最佳算法和理想驱动力的解决方案之间的差异远小于最小规范最小正方形溶液和理想驱动力之间的差异。

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