AEROSPACE CONTROL 2005 Vol.23 Issue 1

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航天控制
AEROSPACE CONTROL

Year 2005 Volume 23

Issue 1

wei hang tian kong zhi de ji shu fan rong er nu li (为航天控制的技术繁荣而努力)

HOU Xiong

.................. page:1-1

Conception on GNC System for Lunar Satellite (月球卫星GNC系统方案设想)

ZONG Hong, Li Tieshou, Wang Dayi

.................. page:2-6

General Research of Satellite Navigation System and the Simulation of an Improved Plan of Constellation (导航卫星系统总体研究及星座改进方案仿真)

Liu Bintao

.................. page:7-10,57

Attitude Control During Lunar Satellite Orbit Maneuver (探月卫星变轨时的姿态控制研究)

Wang Zhai, Li Tieshou, Wang Dayi

.................. page:11-14,40

Preliminary Conception on Propulsion Systems for Chinese Lunar Exploration Project (探月工程中推进系统的初步设想)

Wei Yanming, Ren Kun, Zhang Bing

.................. page:15-22

Error Analysis of a Double-star Attitude Determination Method (一种双星定姿方法的误差分析)

Cheng Yingrong, Zhang Yiqun

.................. page:23-26

Decentralized Coordinated Attitude Control for Large Satellite Formation (大型卫星编队的分布式协同姿态控制)

Xue Dan, Cao Xibin

.................. page:27-30,50

Some Problems of Deep Space Detector Position on Special Point in Solar System (深空探测器定位在太阳系中特殊点上的有关问题)

Wang Haihong, Liu Lin

.................. page:31-34

High-reliability Triple Redundancy Servomechanism System (高可靠三冗余伺服机构系统)

Zeng Guangshang, Shen Weiguo, Shi Li, Zhang Xiaosha

.................. page:35-40

Research and Application of Optimal Nonlinear Control Theory in Missile Control (最优非线性控制技术在导弹控制中的研究与应用)

Sun Zhaogen

.................. page:41-44

Optimal Route Planning Algorithm and Simulation for Low Altitude Penetration (低空突防最优航路规划算法与仿真)

Mu Xiaomin, Jiang Zhichao, Bao Yiming, Wu Sentang

.................. page:45-50

Research on the Method for Designing Interceptor Fuzzy Controller (基于模糊控制的拦截弹姿态控制器设计方法研究)

Bao Wei, Yang Ming, Wang Zicai

.................. page:51-57

Design of Control Signals of Terminal Snake Maneuver for Anti-ship Missiles (反舰导弹末端蛇行机动的控制信号设计)

Gu Wenjin, Zhao Hongchao, Wang Fenglian

.................. page:58-61,64

Cruise Missile Terminal Jump- dive Trajectory Design with Specific Incident Angle (指定入射角的飞航导弹末段俯冲弹道设计)

Sun Mingwei, Peng-Nannan, Wei Yiyin, Yang Ming

.................. page:62-64

A Method of Determining Intercepting Orbit (一种拦截轨道的确定方法)

Cheng Long, Chen Yong

.................. page:65-68

Design of Large-space Variable Trajectory for Anti-ship Missiles Based on Virtual Target (反舰导弹基于虚拟目标的大空域变轨弹道设计)

Zeng Jiayou, Zhao Hongchao, Pan Changpeng

.................. page:69-71,75

The Research of Real-time and Segmented Error Compensation of Gyroscope in SIMU (速率捷联惯导系统陀螺仪误差分段补偿技术研究)

Liu Bo, Li Xuefeng

.................. page:72-75

Semi Physical Simulation Technique about the RF/IR Dual-mode Integrated Homing Guidance System (关于射频与红外复合寻的制导系统的半实物仿真技术)

Wang Chaoqun

.................. page:76-78

Dynamic Simulation of Spacecraft Appendages Deploying (航天器附件展开动力学仿真)

Chen Tong, Xu Shijie

.................. page:79-83

Long-range Fault Location of Long-range Test Launch and Control System During Unmanned Time (远程测发控系统在无人值守期间对部分故障的远程定位)

Jin Zhichao, Huang Lili

.................. page:84-86

Several Critical Problems about Ultra- Violet Lunar Sensor for Lunar Exploration Mission (紫外月球敏感器的几个关键问题)

Hao Yuncai, Wang Li

.................. page:87-91

Study on Position Feedback Correcting Method of Rudder Servo System (舵机伺服系统位置反馈校正方法研究)

Han Jing, Li Gaofeng

.................. page:92-96

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