Hardware in the loop simulation of an attitude control system

被引：0
|
作者：
Leite, WC [1 ]
Mallaco, LMR [1 ]
Carrijo, DS [1 ]
机构：
[1] Inst Aeronaut & Espaco, Space Syst Dept, BR-12228904 Sao Jose Dos Campos, SP, Brazil
来源：
AIAA MODELING AND SIMULATION TECHNOLOGIES CONFERENCE: A COLLECTION OF TECHNICAL PAPERS | 1999年
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
In this work, part of the hardware in the loop simulation of the Brazilian Satellite Launcher VLS attitude control system is described. This particular attitude control system aims to point the last stage of the launch vehicle, prior to its ignition, in order to inject a satellite in a specified orbit. The main result is the final positioning accuracy of the pointing system, which matched the specification The detailed simulation scheme is presented as well as the simulation results.
引用
收藏
页码：423 / 426
页数：4
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