Autonomous Functions of NOZOMI Attitude and Orbit Control System and Mars Imaging Camera
スポンサーリンク
概要
- 論文の詳細を見る
NOZOMI spacecraft was launched on July 4 (JST), 1998 toward Mars. Due to some malfunctions in orbit, NOZOMI unfortunately could not be entered into Martian orbit and expected observation missions around Mars were not performed. However, some autonomous or automatic functions which were prepared to realize the missions were demonstrated ill orbit. This paper describes the autonomous or automatic control functions of NOZOMI AOCS (Attitude and Orbit Control System) and the autonomous imaging function of MIC (Mars Imaging Camera). AOCS autonomous functions were very useful in real in-orbit operation after the telemetry function had lost. The autonomous imaging function of MIC was tested using Moon as a tracking target.
- 特定非営利活動法人 日本ロケット協会の論文
特定非営利活動法人 日本ロケット協会 | 論文
- Current Status of Rocket Developments in Universities -Development of a Small Rocket without Combustion Process
- Cost Comparison between HEO Satellites and 3G Wireless Mobile Phonos for Nationwide Ambulance Network
- The Avionics System Design Concepts for the Advanced Solid Rocket
- Autonomous Functions of NOZOMI Attitude and Orbit Control System and Mars Imaging Camera
- Precise Orbit Determination for ALOS and the Accuracy Verification by SLR