Generally , the amplitude of the acceleration from the perpendicular direction is higher than that from the longitu dinal 但在高速經過類似三角形凸塊時受到離散激勵,縱向加速度峰值明顯高于垂直加速度。
Based on the mathematical model developed by the paper , the trim calculations are carried out in the conditions that the example aircraft converts from helicopter to airplane mode in level flight with zero longitudinal acceleration and angular rate 本文依據所建立的樣例機縱向動力學模型,假定飛機在給定高度平飛,縱向加速度和角加速度均為零,完成過渡模式下的動力學配平。