Aerospace Control 2002 Issue 3 Attitude Determination Using Double Star System

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Aerospace Control
1006-3242
2002 Issue 3

Attitude Determination Using Double Star System
zheng qing zuo ; zhang yu lin

..............page:1-6,76

Spacecraft Integrated Attitude Determination Based on GPS/IMU/Sun Sensor
yang jing ; zhang hong zuo ; wei chun ling

..............page:7-13

Observability's Comprehensive Analysis of Inertial Navigation System
wang xin long ; shen gong xun

..............page:14-19

A New Design Approach for Air Defense Missile Autopilot Based on Genetic Algorithms and Artificial Neural networks
bei chao ; zhou feng zuo ; zhou jun

..............page:20-26

Fault Diagnosis in Attitude Control System of Missile Based on Neural Network
li jiong ; huang shu cai

..............page:27-31

Autononous Navigation Techniques for Spacecraft Rendezvous
wang xu dong ; li guo ; xie bin

..............page:32-38

Autonomous Navigation Design for Small Satellite Using Earth Magnetic Field Measurement
wang jian zuo ; cao xi bin

..............page:39-43

Formation Flying Dynamics of Small Satellites and It's Application
zhang zhen min ; lin lai xing

..............page:44-50

Constellations and Their Orbit Control Techniques
pan ke yan ; wang xu dong ; li guo

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

Newly Established Equation of Flyback Converter(FRE. Given) and Its Analytical Solution
sun ding hao

..............page:58-65

Ballistic Simulation Model of the Missile with Three Aisles Based on the Sirnulink Toolbox
zhang tao ; peng shao xiong ; nie yong fang

..............page:66-70

An Simulink Study of Active- Controlling Duffing Chaotic System by Using Feedback Method
han bao hong ; zuo shi ; cui kun lin

..............page:71-76

Study on Reliability Design of Flight Control Software
ma wei hua

..............page:77-81