1.
Integrated Flight/Propulsion Control Simulation Test Platform and Its Monitoring System Design;
飞/推综合控制半物理仿真平台及监控系统设计
2.
Optimization Computer Design of Integrated Flight and Propulsion Control Based on Double DSP System;
基于双DSP平台的飞/推综合控制优化计算机设计
3.
Design of Monitoring System for Integrated Flight/Propulsion Control Simulation Platform and Study on Simulation Technology;
飞/推综合控制仿真平台监控系统设计及仿真技术研究
4.
Optimization Computer Design of Integrated Flight and Propulsion Control Based on DSP and CAN-bus;
基于DSP和CAN总线的飞/推综合控制优化计算机设计
5.
The Ameliorative Design of Integrated Flight/propulsion Control Computer and The Optimization of Control Parameter;
飞/推综合优化计算机改进设计及控制参数优化
6.
Controller partitioning method for integrated flight/vectoring propulsion control
综合飞行/矢量推进系统控制器分离方法
7.
Integrated flight-propulsion control for ramjet vehicle
以冲压发动机为动力的飞行/推进综合控制
8.
Research on Robust Control Method for Uncertain Nonlinear Integrated Fire/Flight/Propulsion System;
不确定非线性综合火力/飞行/推进系统鲁棒控制方法研究
9.
The Study of Distributed Simulation Environment for Integrated Fire/Flight/Propulsion Control System;
面向火力/飞行/推进综合控制系统的分布仿真环境研究
10.
Integrated reconfigurable flight control method for aircraft with multiple control effectors
多操纵面飞机综合重构飞行控制方法
11.
Study on Flight Control Law Based on Synthesized Nonlinear Control method
基于综合非线性控制方法的飞行控制律研究
12.
The Integrated Design of Fuzzy Logic and Data Acquisition System for Micro Aerial Vehicle;
微型飞行器模糊控制及信号采集系统综合设计
13.
The Synthesized Nonlinear Control Method Based on Nonlinear Inverse Dynamics Control
基于动态逆的综合非线性飞行控制方法
14.
Research on the Data Integration in the Aircraft Control System
飞行器控制系统数据综合关键技术研究
15.
Differential Game Method of Attitude Control System Synthesis for Flight Vehicle
飞行器姿态控制系统综合的一种微分对策方法
16.
The Design and Simulation of Non-guided Weapon Integrated Fire & Flight Control System for Attack Helicopter;
武装直升机非制导武器综合火力/飞行控制系统设计与仿真
17.
Derivation of Linearization Small Deviation Equations and Design of Compound Control System for Aid-sliding Vehicles
助推滑翔飞行器复合控制系统线性化小偏差运动方程推导与控制系统设计
18.
On the basis of aircraft model and propulsion model, post stall flight simulation on routine engine control and engine stability control was accomplished.
推力矢量参与飞行控制，提高了飞机过失速飞行控制能力。