To avoid high frequency oscillation in the course of autopilot design, damping coefficient value was treated as a constraint, the rise time was taken as objective, and the other performance criteria were taken as constraints, then the robustness design pr
To avoid high frequency oscillation in the course of autopilot design, damping coefficient value was treated as a constraint, the rise time was taken as objective, and the other performance criteria were taken as constraints, then the robustness design pr
摘要在导弹控制系统设计过程中，考虑了自动驾驶仪的高频振荡问题，将其转化为系统的一个约束条件，同时把上升时间转化为目标函数，其他设计指标视为约束条件，采用有约束多目标优化的方法解决了系统鲁棒性设计问题。