扰动的出现影响了透射偏振光的质量。
The general time-dependent SchrOdinger equation with external perturbance needs to be resolved through Lie group decompositions.而一般具有外加微扰作用力的含时薛定谔方程的求解需要通过李群分解。
Taking initial aiming error as inertial small perturbance, we established a model of guidance loop with velocity pursuit guidance law at the ideal conditions and deduced an analytical expression.针对大离轴发射条件下的近距格斗导弹,分析了大离轴制导的要求,提出了适用于大离轴制导阶段的快速转弯制导律,并进行了推导及分析。