It will include the completion of the Vertical Launch Complex facility, two visitor centres in nearby towns and a further visitor centre on the main spaceport site. 这包括复杂的垂直发射设备,附近城镇两座游客中心以及一个在主宇航中心的游客中心的建成。
The major task of satellite environment control is to guarantee that the satellite tested in launch complex is kept in the environment as required in terms of temperature, humidity, cleanliness, vibration, ect. 卫星环境控制的主要任务是确保卫星在发射场测试期间,始终工作在符合卫星要求的温度、湿度、洁净度、振动等环境之中。
The movable service tower in satellite launch centre is a steel structure tower which serves satellite launch. The tower has a irregular plane, complex modle and can be moved. The design method of the tower structure is presented with programme SST. 某卫星发射中心活动勤务塔为钢结构塔架,结构平面不规则,型式复杂且可移动,塔架的设计计算采用专用的SST程序,计算结果表明,设计控制荷载为风荷载。
A steel box-section crane girder with 4m high and 1.7m width are manufactured for a launch out dock. The large section and height and the complex fabrication technics of it are infrequent in the engineering of China. 某动力公司出海口基地码头的一高4000mm、宽1700mm的钢箱型吊车梁,截面之大、重量之重在国内很罕见,其制作工艺较为复杂。
In the process of handling, transport, launch and flying, the space vehicles are always in the complex environment of mechanics, for example, the vibration and impact are the important influence. 在装卸、运输和发射、飞行的过程中,飞行器要经历复杂的力学环境,以振动和冲击环境最为典型。
The comparison between fuzzy controller and PID controller proves that the former is better than the latter in respect of dynamic properties and robustness. And therefore it is exceptionally applicable to the control system of spacecraft launch complex. 并将模糊控制器与PID控制器的动态特性进行了比较,证实了模糊控制器较PID控制器有更好的动态控制特性和鲁棒性,特别适合在航天器发射场控制系统中应用。
In order to launch missile rapidly and movably under complex application environment, Information-based missile-launcher requests the navigation system not only to be accurate in providing the navigation information, but also to be high reliable, independent and anti-jamming. 导弹信息化机动发射平台的应用环境非常复杂,为了能够实现导弹的快速机动发射,不仅要求导航系统能够提供高精度的导航信息,还要求导航系统具有高度的可靠性、自主性和抗干扰性。
Discussed in detail the principle of these two scenarios and problems that may exist, the common feature of both scenarios: ask for much of the launch system and detector, simple operation, do not need complex control circuits. 本文详细探讨了这两种方案的原理及可能存在的问题,两种方案共同的特点是:对发射系统和探测器的要求不高、操作简单、不需要复杂的控制电路。