Angular Momentum Reduction Using Mechanical Impulse for Uncontrollable Satellite Capturing
スポンサーリンク
概要
- 論文の詳細を見る
A method for reducing the angular momentum of a non-cooperative, free-flying object in orbit by the application of repeated, well-timed impulses is studied. Using numerical simulations it has been shown that nutation or tumbling can be converted into simple spin or stopped altogether by this technique, which is robust against errors in the applied force. Owing to uncertainties in the projectile-target collision-force profile, ground experiments have been conducted using a passive model satellite placed on an air table. A mechanism for providing impulses to a target is described in this paper.
- 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