meetings - Space Flight Mechanics Committee
meetings - Space Flight Mechanics Committee
meetings - Space Flight Mechanics Committee
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13-406 Being Lost in <strong>Space</strong><br />
Yuya Mimasu, Japan Aerospace Exploration Agency; Sho Taniguchi, Fujitsu<br />
Limited; Hiroshi Takeuchi, Japan Aerospace Exploration Agency; Yoji Shirasawa,<br />
Japan Aerospace Exploration Agency; Osamu Mori, Japan Aerospace Exploration<br />
Agency; Ryu Funase, Japan Aerospace Exploration Agency; Takanao Saiki, JAXA /<br />
ISAS; Yuichi Tsuda, Japan Aerospace Exploration Agency<br />
The world’s first solar sail IKAROS (Interplanetary Kite-craft Accelerated by Radiation Of<br />
the Sun) which is operated by Japan Aerospace Exploration Agency (JAXA) lost<br />
communication with the ground station due to the power shortage on December 24, 2011.<br />
In order to acquire IKAROS again after the power comes back, we immediately initiated to<br />
predict the attitude and orbit for the spacecraft. As the result of the effort for the prediction,<br />
finally we acquire IKAROS after 9 months. This paper presents that the attitude and orbit<br />
prediction technique, while IKAROS was lost in space.<br />
16:15 AAS In-<strong>Flight</strong> Aerodynamic and Mass Properties Identification Design for Mars<br />
13-407 Aerobraking<br />
Ling Jiang, Beihang University<br />
Aerobraking is a revolutionary technique that has been used successfully in recent Mars<br />
missions. But consideration of significant risk and cost has led to the development of<br />
autonomous aerobraking design. This paper proposes a novel method of estimating varying<br />
aerodynamic and mass properties in-flight to improve the onboard capacity for corridor<br />
controller design. The identification approach is divided into two steps: executing mass<br />
properties identification at the apoapsis walk-in and adjustment maneuvers first, and then<br />
implementing aerodynamic property estimation during atmospheric passes. Simulation<br />
results show that the proposed approach is simple and effective, making it suitable for on-<br />
Page 84<br />
23 rd AAS / AIAA <strong>Space</strong> <strong>Flight</strong> <strong>Mechanics</strong> Meeting