針對(duì)飛行模擬機(jī)運(yùn)動(dòng)載荷系統(tǒng)中平臺(tái)質(zhì)心處的線加速度的算法進(jìn)行了剖析，并就液壓伺服作動(dòng)筒的伸縮長(zhǎng)度與飛機(jī)特定力和飛機(jī)轉(zhuǎn)動(dòng)率之間的關(guān)系進(jìn)行了分析。提出了運(yùn)動(dòng)方程建模的依據(jù)，探討了模擬機(jī)六自由度運(yùn)動(dòng)系統(tǒng)在軟硬件上的合成原理，為飛行模擬機(jī)液壓伺服控制在運(yùn)動(dòng)系統(tǒng)過(guò)載保護(hù)性能方面的改善及研究打下了基礎(chǔ)。
關(guān) 鍵 詞 線性通道; 角度通道; 質(zhì)心變換; 旋轉(zhuǎn)率

Abstract The present essay dissects the algorithm of the linear acceleration at the centre of gravity of the platform of the motion loading system, and also analyses the relations of hydraulic servo actuator’s travel distance, the aircraft’s specific force and the aircraft’s rotational rate. The essay also suggests the basis of motion equation modeling, and discusses the simulator’s six-degree-of-freedom motion system’s combination principles by the means of the hardware and software, and all these make the foundation of the research of flight simulator hydraulic servo control in improving performance of overload protection.
Key words linear channel; angular channel; centroid transition; rotational rate