Active Attitude Control of Large and Flexible Space Structure Using Solar Radiation Pressure

利用太阳辐射压对大型柔性空间结构主动姿态控制

• 批准号: 20860098
• 负责人: FUNASE Ryu
• 金额: $ 2.1万
• 依托单位: Japan Aerospace Exploration Agency
• 依托单位国家: 日本
• 项目类别: Grant-in-Aid for Young Scientists (Start-up)
• 财政年份: 2008
• 资助国家: 日本
• 起止时间: 2008 至 2009
• 项目状态: 已结题
• 来源: https://kaken.nii.ac.jp/grant/KAKENHI-PROJECT-20860098/
• 关键词: 柔軟宇宙構造物; 大型宇宙構造物; 姿勢制御; 太陽光圧; 制御工学

The objective of this research is to realize the active control system to control the attitude of large and flexible space structure using solar radiation pressure. As a target of this research, attitude control of spinning solar sail spacecraft is selected, which deploys huge and flexible thin membrane in space and uses the radiation pressure by the sun light's reflection as its propulsive force. A film-type device which can control its optical parameter was developed in this research. Unbalance of the solar radiation pressure generated by the device can apply minute and continuous control torque to the sail so that very stable attitude control of large and flexible structure is realized. The developed attitude control device is attached to the sail of "IKAROS" solar sail spacecraft which was launched in 2010. The proposed attitude control system will be demonstrated by applying this device as a means of attitude control of IKAROS spacecraft.

这项研究的目的是实现主动控制系统，以使用太阳辐射压力来控制大型柔性空间结构的态度。作为这项研究的目标，选择了旋转太阳能航天器的态度控制，该航天器在太空中部署了巨大而柔软的薄膜，并利用太阳光的反射作为其推进力。在这项研究中开发了一种可以控制其光学参数的膜型设备。设备产生的太阳辐射压力的不平衡可以在帆上施加微小和连续的控制扭矩，从而实现了对大型柔性结构的非常稳定的态度控制。开发的态度控制装置附在2010年推出的“ Ikaros”太阳能航天器的帆中。提议的态度控制系统将通过应用此设备作为Ikaros航天器的态度控制的手段来证明。

项目成果

Oscillation-Free Attitude Control of Spinning Solar Sail with Huge Flexible Membrane

巨型柔性膜旋转太阳帆的无振荡姿态控制

• 发表时间: 2009
• 作者: Mitsuyasu Iwanami;Yuichiro Kawabata;ほか3名;Osamu Mori;Yuya Mimasu;Ryu Funase;Ryu Funase;Ryu Funase
• 通讯作者: Ryu Funase

Attitude Controller Design for Spinning Solar Sail Using Analytical First-Order Oscillation Model and Numerical Multi-Particle Model

使用解析一阶振荡模型和数值多粒子模型的旋转太阳帆姿态控制器设计

• 发表时间: 2009
• 作者: Mitsuyasu Iwanami;Yuichiro Kawabata;ほか3名;Osamu Mori
• 通讯作者: Osamu Mori

Photon Acceleration Model of Flexible Spinning Solar Sail

柔性旋转太阳帆的光子加速模型

• 发表时间: 2010
• 期刊: TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
• 作者: Yuko Nitahara-Kasahara;et. al.;菅野美佐子;Yuya MIMASU
• 通讯作者: Yuya MIMASU

Estimation of Solar Radiation Pressure Parameters for Solar Sail Demonstrator IKAROS Considering Attitude Dynamics

考虑姿态动力学的太阳帆演示器 IKAROS 太阳辐射压力参数估计

• 发表时间: 2010
• 作者: 池田隆徳;濱田秀則;佐川康貴;川端雄一郎;山田一夫;Ryu Funase;Yuya Mimasu
• 通讯作者: Yuya Mimasu

Solar Radiation Pressure Model for Attitude Motion of Hayabusa in Return Cruising

隼鸟返航姿态运动的太阳辐射压力模型

• 发表时间: 2009
• 作者: Mitsuyasu Iwanami;Yuichiro Kawabata;ほか3名;Osamu Mori;Yuya Mimasu
• 通讯作者: Yuya Mimasu