A solution of the navigation problem for autonomous insertion of payload into a geostationary orbit using a low-thrust engine

被引：3

作者：

Kozorez, D. A. ^{[1
]}

Krasil'shchikov, M. N. ^{[1
]}

Kruzhkov, D. M. ^{[1
]}

Sypalo, K. I. ^{[1
]}

机构：

[1] Natl Res Univ, Moscow Aviat Inst, Moscow 125993, Russia

来源：

JOURNAL OF COMPUTER AND SYSTEMS SCIENCES INTERNATIONAL | 2015年 / 54卷 / 01期

关键词：

GNSS; System Science International; Thrust Vector; Navigation Problem; GNSS Receiver;

D O I：

10.1134/S1064230715010086

中图分类号：

TP18 [人工智能理论];

学科分类号：

081104 ; 0812 ; 0835 ; 1405 ;

摘要：

An onboard navigation system for a space vehicle (satellite) as it is inserted into a geostationary orbit using a low-thrust engine is considered. The navigation system uses optoelectronic Earth, Sun, and star sensors and a multichannel GNSS signal receiver. The purpose of the study is to form a general design of the integrated navigation system, including the justification of its architecture and operation algorithms, based on requirements for the accuracy of the navigation problem solution. To integrate various measurements, a quasilinear Kalman filter and its special "scalar" modification are used. The vector to be estimated onboard the spacecraft consists of the coordinate and velocity components, the attitude of its body axis, and the attitude and actual thrust of its main thruster. Instrument sensor errors are considered as uncontrollable factors. The main tool for the analysis of the navigation system error is simulation, which is performed using dedicated software developed using the object-oriented paradigm.

引用

页码：104 / 115

页数：12

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