satellite system design

Height measuring by master satellite and concomitant satellite formation InSAR system being the background, the problem of the concomitant satellite formation configuration optimal design is studied.

以主星&辅星编队InSAR系统干涉测高为应用背景，研究辅星编队的优化设计问题。

Satellite beam synchronization design strategy is key design issue of distributed spaceborne radar system design.

波束同步设计是星载分布式雷达系统总体设计的重要问题。

Satellite System Design Optimization Based on STK

基于STK的卫星系统设计优化研究

Design of Refrigerating and Vacuum System of the Test-Bed for Heat Tube in Artificial Satellite

卫星热管传热测试台的制冷与真空系统的设计

Contented Based Cloudy Satellite Images Retrieval System Design and Practice

基于内容的卫星云图检索系统设计与实现

Some Hotel's Technology Analysis and Design of Satellite Communication and Community Antenna System

某宾馆卫星及共用天线系统技术分析与设计

The position theory of underwater mobile vehicle based on satellite positioning technology is studied, and the vehicle positioning algorithm is analyzed too. A design of underwater cooperant beacon monitoring system based on DSP, GPS and wireless communication technology is introduced.

研究了基于卫星定位技术的水下移动目标定位原理，分析了目标的实时定位算法，提出了一种基于GPS技术、DSP技术和无线通信技术的水下合作目标监控系统设计方案。

Results Taking the gyrostabilizer system of ×× satellite for example, the dynamic equations were solved under giving initial conditions using the Runge-Kutta numeric method, investigate the dynamic optimization design for the gyrostabilizer system.

结果以××航天器天线姿态稳定系统为例，在给定初始条件下用Runge Kutta数值方法对系统的动力学模型进行了数值仿真，从而为陀螺机构的动力学优化设计奠定了基础。

In order to simplify the control of tethered satellite system ( TSS), a new design method was proposed by upgrading the existing methods.

为了简化绳系卫星系统（TSS）的控制，对已有的设计方法进行了改进，提出了一种新的控制律设计方法。

Parameter optimization of satellite system is a typical problem of MDO ( Multidisciplinary Design Optimization ).

卫星总体参数优化是一个典型的多学科优化问题.

Based on three-axis stabilized satellite attitude control system, a fault detection approach is presented and a relevant simulation is given to show the design procedures and illustrate the effect of the proposed approach.

本文针对三轴稳定卫星的姿态控制系统研究了其故障检测算法，并通过仿真验证了所提算法的有效性。