The flying saucer is a certain statically unstable system, and with the model bias, the conventionally designed predictive control system is hard to get ideal control effect.
碟形飞行器是一类较为特别的静不稳定系统,在系统数学模型存在较大偏差的情况下,常规的预测控制设计思路难以获得理想控制效果。
According to the classical control theory, this paper deals with two designs of critical statically unstable attitude control system.
根据经典控制理论,设计了两类临界静不稳定姿态控制系统。
应用推荐