USING KANES METHOD TO FORMULATE DYNAMIC EQUATIONS OF PASSIVE CONTROLLER OF ROCKET

陈璧辉

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USING KANES METHOD TO FORMULATE DYNAMIC EQUATIONS OF PASSIVE CONTROLLER OF ROCKET

更新时间：2026-09-14

- USING KANES METHOD TO FORMULATE DYNAMIC EQUATIONS OF PASSIVE CONTROLLER OF ROCKET
- 用KANE法建立火箭被动控制动力学方程
- Issue 2, Pages: 140-144(1993)
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- Published：1993
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陈璧辉. USING KANES METHOD TO FORMULATE DYNAMIC EQUATIONS OF PASSIVE CONTROLLER OF ROCKET[J]. 1993, (2): 140-144.
DOI：

陈璧辉. USING KANES METHOD TO FORMULATE DYNAMIC EQUATIONS OF PASSIVE CONTROLLER OF ROCKET[J]. 1993, (2): 140-144. DOI：

摘要

本文介绍用Kane法建立无控火箭被动控制动力学方程。实际被动控制系统简化为12自由度的多刚体模型。选取相对角速度为广义速率得到偏角速度、偏速度。最后通过给出的广义惯性力、广义主动力建立用张量-矩阵记法表示的动力学方程。本文所建立的动力学方程已在山西省计算研究中心的M-240D大型机上通过

计算结果与实测值吻合。

Abstract

By means of Kane's method the dynamic equations of passive controllers on rock- et launchers are introduced. The real system of the passive controllers is simplified to a twelve degree-of-freedom system model. The relative angular velocities are selected as gener- alized speeds to obtain the partial angular velocities and partial velocities. Generalized inertial forces and generalized active forces are discussed. The dynamic equations using tensor/ma- trix expression are formulated. The dynamic equations has been solved on a M-24OD com- puter in the Province Computing Centre of Shanxi. The calculating results are identified with the experimental results.

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ROCKET/LAUNCHER PASSIVE CONTROL TECHNOLOGY

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ASYMPTOTIC BEHAVIOR AND BOUNDEDNESS OF SECOND-ORDER FUNCTIONAL DIFFERENTIAL EQUATIONS WITH APPLICATION TO ROCKET PROPULSION

THE INFLUENCE OF RANDOM VIBRATION OF MULTIPLE ROCKET LAUNCHER TO VOLLEY BOMBING DENSITY

《中北大学学报(自然科学版》》征稿简则

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