CanSat Descent Control System Design and Implementation

被引：0
|
作者：
Kizilkaya, Muhterem Ozgur [1 ]
Oguz, Abdullah Ersan [2 ]
Soyer, Suleyman [3 ]
机构：
[1] Minist Natl Def, Air Force Maintenance Ctr 3, Ankara, Turkey
[2] Turkish Air Force Acad, Elect Eng Dept, Istanbul, Turkey
[3] Turkish Air Force Acad, Aeronaut & Astronaut Engn Dept, Istanbul, Turkey
来源：
PROCEEDINGS OF 8TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES (RAST 2017) | 2017年
关键词：
CanSat; Descent Control; Mars Glider;
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The aim of this study is to design a descent control system for a CanSat that simulates a sensor payload travelling through a Martian atmosphere and sampling the atmospheric composition during flight. CanSat is a first step in space studies that gives low cost opportunity to test the space program design. The system is developed under the rules of International CanSat Competition 2016, which aims to simulate the Mars glider project of NASA. A novel descent control system approach was designed and implemented with cadets according to the requirements of the competition.
引用
收藏
页码：241 / 245
页数：5
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