1) integrated guidance and control
制导一体化
3) integrated guidance and control
制导控制一体化
1.
The problem of integrated guidance and control for BTT missiles is studied.
首先建立了俯仰通道的制导控制一体化状态模型,然后利用特征结构配置方法,设计了导弹制导与控制一体化状态反馈控制律,所设计的控制器一方面保证导弹打击精度,另一方面保证导弹的控制回路的稳定。
2.
According to the kinetic characteristic of the guided bomb with SINS/GPS,the integrated guidance and control model of the pitch plane is formulated firstly.
根据SINS/GPS制导炸弹动力学特性,首先推导了俯仰通道的制导控制一体化状态模型。
4) guidance-fuze integration
引信制导一体化
5) integrated guidance/autopilot
控制导引一体化
1.
Sliding mode control based on NBF net to integrated guidance/autopilot design for missiles;
基于NBF网络的导弹航向平面滑模控制导引一体化
2.
A new approach to integrated guidance/autopilot design for missiles against maneuvering targets on the sea is considered in this study.
提出了一种反舰导弹针对水面机动目标的航向平面控制导引一体化设计方案。
6) centralized leading sys-tem
一元化领导体制
补充资料：波束制导(见遥控制导)
波束制导(见遥控制导)
beam-rider guidance
boshu zhidao波束制导(beam一rider guidanee)见遥控制导。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条