| 1. | Sim / usim detection after turning flight mode off
将飞行模式关闭后的sim / usim卡检测。 |
| 2. | The vessel had two flight modes
它有两种飞行模式。 |
| 3. | Fma flight mode annunciator
飞行方式显示器 |
| 4. | Mobile phone pdas must be switched to " flight mode " when used onboard
于机上使用兼具手机功能的pda时，必须选用flight mode 。 |
| 5. | In this paper , influences that the attack conditions and the flight modes of the fighter and the missile make on the attack effect are discussed focusing on the fighter attack phases
本文主要着眼于飞机实施攻击的阶段，结合近距空地攻击的特点，对飞机和导弹的攻击条件以及飞机攻击方式对攻击效果的影响作了详细的研究。 |
| 6. | There are two aspects introduced firstly : some typical flight modes and several differential geometrical methods . then the latter are respectively used to solve the control problems in those relevant flight modes
本文也对几种利用微分几何理论来解决非线性系统控制问题的方法作了简要的说明，作为必要的数学理论基础。 |
| 7. | Compared with non - slung - load flight , additional aerodynamic load , gravity load should be considered in the slung - load system . so the moment to the gravity center , flight mode and the natural frequency will change
直升机吊挂飞行,与直升机非吊挂飞行状态相比,增加了新的气动载荷、重力载荷,和因此产生的对直升机重心的力矩,其飞行运动模式、低频振荡固有频率均发生改变。 |
| 8. | It is one of the hottest international research topics for the small unmanned helicopter to be controlled , whose flight mode currently is limited mainly by remote controlled , while the research of automated flight control is on the rise
对小型无人直升机的飞行控制目前是国际上的一个研究热点。无人直升机的控制方式主要局限于遥控飞行,对自主飞行控制的研究则方兴未艾。 |
| 9. | There are a variety of flight modes of fighters when they launch air - to - surface ( as ) missiles . since the attack effect determined by fighters , missiles and the characters of the targets , it may vary due to the attack mode of the fighters
飞机与导弹相配合实施近距空地攻击时，尽管飞机实施攻击的飞行方式不同，但是由于攻击效果主要受飞机、导弹武器系统和目标特性限制，因此不同的攻击方式会产生不同的攻击效果。 |
| 10. | By the use of “ radar target backscattering simulation software ” and through many flight mode and research mode experiments with the u . s . - made helicopter ah - 64 as an example , a detailed analysis of helicopter echoes ’ time , frequency domain and time - frequency distribution characteristics is made . finally , according to these features , a tentative plan to detect hovering helicopters is proposed
本文利用专门的电磁仿真软件，以美制“阿帕奇”直升机为例，详细分析了直升机雷达回波的时域、频域和时频分布的特性，并根据这些特点提出了雷达探测武装悬停直升机的初步方案。 |
