研究了超机动飞行推进系统稳定性控制。
A study of propulsion system stability control for super maneuvering flight was carried out.
这一方法主要应用于自主式机动飞行器。
文提出一种关于再入飞行器程序机动飞行的制导方案。
Programming maneuvering flight guidance scheme about reentry vehicle is presented in this paper.
本文对筋斗和横滚机动飞行的运动学问题进行了分析。
The kinematics of helicopters in loop and roll maneuvers is analysed in this paper.
从飞机设计的角度分析了过失速机动飞行的操纵要求问题。
From the viewpoint of aircraft design, a topic on control design requirements for post stall maneuvering is tackled.
当目标作非机动飞行时，最优制导律是变比例系数的比例制导。
When targets flight with zero load-factor, it is a changeable proportional factor guidance law.
在理论和试验上验证了光学引导系统跟踪机动飞行目标的优越性。
The advantage of optical guiding system used in the mobile aero-target tracking is proved in theory and test.
结果表明，过载反馈系统在再入机动飞行器的飞行控制中效果较好。
The results shows that the overload feedback structure is better than the attitude feedback structure on the maneuverable flight control.
当目标作非机动飞行时，最优制导律是一种变比例系数的比例制导。
When targets fly with non-maneuvering, the optimal guidance law is the proportional guidance law with a changeable factor.
高速大迎角动态气动特性是衡量新一代高机动飞行器性能的重要参数之一。
Dynamic aerodynamics characteristic is one of very important parameters of modern maneuverable aircraft to be scaled at high Angle of attack and high speed.
说明了当代战斗机的作战环境和作战方式以及由此提出的大迎角机动飞行的背景。
O. a; explains the mission's environment and fashion of current generation fighter; and the background of high A. o.
飞行目标一般沿圆周路径作机动飞行，因而出现了以圆周运动为基础的跟踪滤波器。
Flying targets normally maneuvering on circular paths, which has lead to tracking filters based on circular turns.
分别模拟目标作巡航飞行、平飞加速、跨越障碍机动、水平蛇行机动飞行时的动作。
The target actions of cruise flying, level accelerating, resolving obstacle move, level hunting move flying were simulated.
游标速度，在某些机动飞行过程中，特别是在进近和着陆时，飞机所应保持的预定速度。
BUG speed, a preselected speed to be observed during certain maneuvers, particularly the approach and landing sequence.
旨在揭示机动飞行产生的附加离心力和附加陀螺力矩对裂纹转子系统非线性响应的影响。
It aims to reveal the influence of maneuver load on the nonlinear response of cracked rotor.
针对大气层内的机动飞行目标，提出了一种可用于质量矩拦截器末制导段的比例制导律。
Based on the constructed model of the mass moment interception missile (MMIM), a coupled nonlinear system is presented by rational simplification in this paper.
本文以能量法研究直升机转弯机动飞行特性，这是评价一架直升机机动性能的基本要素之一。
The turning maneuver characteristics are one of the essential factors for evaluating the helicopter maneuver characteristics.
快速控制菜单最适宜玩家在战场上空实行机动飞行操控，随便你看什么，选控系统都能够反映出来。
The quick-command menu is great for reacting to the battle field on the fly, the available options changing to reflect whatever you're looking at.
利用典型状态的风洞试验结果对十字布局与叉字布局再入机动飞行器的气动特性进行了分析与比较。
In this paper aerodynamic characteristics of maneuvering reentry vehicle of cruciform configuration and bifurcate configuration are compared by means of the wind tunnel test results.
本文讨论了高机动性飞机滚转机动飞行对纵横航向操纵效能的要求，并以J-7飞机为算例进行了验证。
The longitudinal and lateral directional control effectiveness requirements of high maneuver aircraft are discussed in this paper, and the fighter J-7 is taken as an example.
可以提供更详细的多学科计算流体动力学的非定常空气动力学过程的认识，涉及现代制导武器系统机动飞行。
Multidisciplinary computations can provide detailed fluid dynamic understanding of the unsteady aerodynamics processes involving the maneuvering flight of modern guided weapon systems.
将各机动飞行任务的同类任务段和同类载荷循环乘以任务混频后进行加权平均即得到机动飞行类综合载荷谱。
After averaging the same flight segments by multiplying mission mix rates, then the weighted mean profiles can be obtained, which represent the composite maneuver flight loading spectrum.
直升机飞行动力学逆问题是研究已知运动的控制规律，对直升机机动飞行和现代飞行控制律设计有重要意义。
Inverse problem of helicopter flight dynamics, to solve control laws from given motion, is important to the study for the maneuvering flight and the design for the advanced flight control system.
仿真计算结果表明，采用脉冲控制模式，本文提出的安全轨迹制导策略能够实现小卫星临近作业的安全机动飞行。
The results of the simulation indicate that the safety trajectory guidance strategy can achieve safety maneuver flying of the small satellite proximity operation when using thrust control method.
以UH 60A直升机在高速飞行条件下的急拉杆机动飞行为例进行仿真计算，并与飞行试验数据进行对比验证。
As an example, a pull-up maneuver of helicopter UH-60A under high speed flight condition is simulated. The correlation of the results with the flight test data is provided.
然而对于英国航空公司来说更令人担心的是，以前大城市之间的传统网络模式越来越趋向低成本航空公司的机动飞行网络。
More worrying for ba, however, is the trend away from conventional route networks based on big hubs to the AD hoc linking of airports by the low-cost airlines.
然而对于英国航空公司来说更令人担心的是，以前大城市之间的传统网络模式越来越趋向低成本航空公司的机动飞行网络。
More worrying for ba, however, is the trend away from conventional route networks based on big hubs to the AD hoc linking of airports by the low-cost airlines.
应用推荐