The pilot's optimal control model is investigated. The optimal design destination function and method of flight controlling system have been proposed.
建立了驾驶员最优控制模型，提出了飞行控制系统优化设计目标函数和设计方法。
Based on 12-state nonlinear aircraft dynamic model, a nonlinear flight control law is designed by using nonlinear inverse dynamics and modern optimal control theory.
针对12维非线性飞机动力学模型，利用非线性逆系统理论和现代最优控制理论设计了一组非线性飞行控制规律。
This paper proposes that it is necessary to concern the pilot's control behavior and human limits during the optimal design of modern flight controlling system.
提出了现代飞行控制系统的优化设计需考虑驾驶员的操纵行为和生理限制，才能进行人-机组合优化设计。
Optimal control of tactical maneuver for a high-performance aircraft is investigated in flight trajectory.
应用轨迹优化方法研究了高性能战斗机机动动作的最优控制问题。
On the aspect of getting the optimal flight performance, this paper discusses the trimming principle and solution for the aircraft with multiple control effectors.
从飞行性能最优的角度，对多操纵面飞机的配平原则与算法进行了研究。
The guidance and control methods should enable the ASV to accomplish fully autonomous and adaptive flight, a key problem is to achieve the optimal controls quickly.
先进航天器飞行时应具备自主导航的能力，其实现的关键技术之一是用机载计算机近实时或实时地生成一条满足各种约束条件的优化轨道。
The guidance and control methods should enable the ASV to accomplish fully autonomous and adaptive flight, a key problem is to achieve the optimal controls quickly.
先进航天器飞行时应具备自主导航的能力，其实现的关键技术之一是用机载计算机近实时或实时地生成一条满足各种约束条件的优化轨道。
应用推荐