The state information and driving order transforms into 1-Wire signal, connecting to the bay controller with a common 1-Wire bus; All bay controllers exchange information with the host computer, realizing the scouting and controlling of the anti-misoperation locks.
新型电磁锁采集的状态信息和驱动命令都转化为单总线信号,共用一条单总线与间隔控制器连接;各间隔控制器通过CAN现场总线与变电站层的主机进行信息交互,实现主机对电磁锁的远程监控。
In the paper the authors point out the essense of direct manipulation in 3D space interaction technology,and discuss the principle and application of 3D space controller with six degrees of freedom whic.
本文指出三维空间交互的直接操纵本质，介绍操纵三维对象所需的六自由度三维空间控制器的原理和应用。
Application of second-order dynamic Terminal sliding mode control based on nonlinear disturbance observer to near space vehicle
基于非线性干扰观测器的二阶动态Terminal滑模在近空间飞行器控制中的应用
Variable Structure Near Space Vehicle Control Characteristics of Large Flight Envelope
变结构近空间飞行器大飞行包络控制特性研究
Study on the Control of Spacecraft Attitude Based on BP Neural Network;
基于BP神经网络的空间飞行器姿态控制研究
A Continuous Nonlinear Robust Control Design for Hypersonic Vehicles
近空间飞行器的连续非线性鲁棒控制设计
Decentralized UAV Formation Tracking Flight Control in Obstacle Laden Environment
障碍空间中的飞行器编队与集群控制研究
Spacecraft Large Angle Maneuver Control Based on Inverse Dynamic
基于逆动态理论的空间飞行器大角度机动控制
PROGRESS IN AERODYNAMICS OF COMBINATION CONTROL FOR VEHICLES AT HIGH SPEED
近空间飞行器的气动复合控制原理及研究进展
Robust Optimal Predictive Control for a Near-Space Vehicle Based on Functional Link Network Disturbance Observer
基于FLNDO的近空间飞行器鲁棒最优预测控制(英文)
Robust Tracking Control of Near Space Vehicle Based on Dynamic Saturation Function Fast Terminal Sliding-Mode
近空间飞行器的DSF:vsat鲁棒快速Terminal滑模控制
Nonlinear Attitude Control of Spacecraft Based on Double-Gimbaled Control Moment Gyroscopes
基于双框架控制力矩陀螺的空间飞行器非线性姿态控制
T-S fuzzy adaptive observer based fault diagnosis and fault tolerant control for near space vehicle
基于模糊T-S自适应观测器的近空间飞行器故障诊断与容错控制
To confirm your flight yoke's center position, leave the yoke centered, and then press one of its buttons.
要确认飞行控制器的中间位置，请将飞行控制器放在中间位置，然后按飞行控制器上的某个按钮。
Also, loads and control forces imposed by space vehicle guidance systems are generally small.
此外，由空间飞行器导引系统所产生的载荷与控制力一般是很小的。
Introduce of Max Power Point Tracking System;
空间飞行器太阳能峰值功率跟踪控制系统（MPPT）研究
Research and Design of a Spacecraft Attitude Control Simulator System;
空间飞行器姿态控制仿真试验平台系统研究与设计
Research on Attitude Control about Aerospace Vehicle Based on Multi-Agent;
基于多Agent的空天飞行器的姿态控制
SSLV (Standardized Space Launch Vehicle)
标准空间发射飞行器
standardized space launch vehicle
标准化空间发射飞行器
