飞行器的例句大全

A virtual proto-type HIL simulation system for spacecraft docking was established.

阐述了飞行器空间对接地面半物理仿真系统设计思想.

The stability of sliding mode in nonlinear system was proven by the nonlinear differential equation.

在此基础上,设计了飞行器模型参考变结构姿态控制系统,并严格证明了系统状态在滑动模态的稳定性.

To maintain normal air pressure in ( an enclosure , as an aircraft or a submarine ).

飞行器的隔离舱中保持的气压.

The decoupled spacecraft with large parameter variations and external disturbances is of good robustness.

在大的参数变化和外干扰下,解耦空间飞行器具有优良的鲁棒性.

A robust decoupling control method for BTT vehicle is proposed.

提出BTT飞行器的一种鲁棒解耦控制方法.

With such a large heat sink value, FRA can meet the requirement of hypersonic flying machine.

在800℃时,两者都具有较高的热沉值,分别达到569MJkg和660MJkg, 该热沉值能够满足超高音速飞行器的热管理要求.

A new method of quickly hypersonic waverider forebody configurations was developed.

发展了一种基于分析法的高超声速乘波构型飞行器前体设计方法.

Metallic thermal protection system a feasible solution for thermal protection of hypersonic vehicles.

金属热防护系统是高超飞行器热防护系统的理想候选方案.

Hypersonic vehicle must be designed in integration methodology for the strong coupling effect of the subsystems.

高超声速飞行器各子系统之间存在着很强的相互作用,这要求在设计过程中必须采用一体化技术.

The forebody design a key issue for hypersonic airbreathing vehicle.

前体设计是吸气式高超声速飞行器设计的关键之一.

In May of that year, Wilbur sailed to France to demonstrate their new Type A Flyer.

那年5月, 威尔伯乘船到法国展示他们新型的“A型飞行器”.

Spacecraft is a complex system that is combined with mechanics, hydraulics, electronics and thermal control.

空间飞行器是集机械 、 液压 、 电子、热控等于一体的复杂大系统.

Military facility for jet fuel transfer from large underground storage tank to aircraft re-fueling hydrant pit.

军用航油运输设施:从地下储油罐到给飞行器加油的现场.

They would inflict no lasting damage to spacecraft and create no debris in orbit.

这些陆基系统不会对空间飞行器造成持久性的伤害并且不会在轨道上生成碎片.

Balloons are aerostats, which means that are lighter than air when inflated.

气球是轻飞行器,也就是说,充气后, 它们会比空气轻.

Since its inception the company has produced 53 different aircraft designs.

该公司自成立以来已经完成了53种不同样式飞行器的设计。

The rotor system locates in an aircraft flying with an asymptotic acceleration.

研究渐变加速的飞行器内碰摩转子系统的非线性特性.

This was the primary reason for selecting the fin size for the Saturn Vehicle.

这就是“土星”飞行器安定面尺寸选择的主要依据.

Affected by unsteady atmosphere disturbance, attitude control and navigation for MAV flight must be unconventional.

针对在非定常大气扰动作用下, 微型飞行器MAV姿态稳定控制与导航都不同于常规的问题.

The guidance, navigation and control ( GNC ) system of micro air vehicle ( MAV ) is constructed.

构建了微小型飞行器 ( MAV ) 导航、制导与控制 ( GNC ) 系统.