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System Techniques, Satellites, Orbit Design, Thermal Control, Power Supply, Attitude Control, Telemetry System

机译：系统技术，卫星，轨道设计，热控制，电源，姿态控制，遥测系统

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A proposal is given for a climate research mission for Earth radiation budget measurements. This requires daily global coverage fulfilled by a system of three orbiting satellites. One of these is on a nonsunsynchronous drift orbit with about 57 deg inclination, represented by the satellite SEOCS. The two others are polar orbiting satellites, called POMS. Appropriate orbits are designed for these and concepts are investigated up to component level in order to demonstrate mission feasibility.

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作者
Puls, J.;
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年度 1979
页码 p.1-164
总页数 164
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Climate; Energy budgets; Meteorological satellites; Polar orbits; Satellite observation; Terrestrial radiation; Feasibility analysis; Mission planning;

机译：气候;能源预算;气象卫星;极地轨道;卫星观测;地面辐射;可行性分析;任务规划;

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专利

1. SATELLITE ATTITUDE CONTROL WITH USING A COMBINED ATTITUDE AND THERMAL CONTROL SYSTEM WITH THE ACTIVE FORCE CONTROL [J] . SALEH BASHA ALKHODARI, RENUGANTH VARATHARAJOO Journal of the British Interplanetary Society . 2010,第7期

机译：结合姿态和热力控制系统以及主动力控制的卫星姿态控制
2. Design of Modular Power Management and Attitude Control Subsystems for a Microsatellite [J] . Ali Anwar, Khan Shoaib Ahmed, Khan M. Usman, International journal of aerospace engineering . 2018,第3期

机译：微卫星模块化电源管理和姿态控制子系统的设计
3. Design of Modular Power Management and Attitude Control Subsystems for a Microsatellite [J] . Anwar Ali, Shoaib Ahmed Khan, M. Usman Khan, International journal of aerospace engineering . 2018,第4期

机译：微卫星模块化电源管理和姿态控制子系统的设计
4. Design, Implementation and In-orbit Demonstration of Attitude and Orbit Control System for Micro-satellite ALE-2 [C] . Yuji Sato, Shinya Fujita, Toshinori Kuwahara, IEEE/SICE International Symposium on System Integration . 2021

机译：微卫星ALE-2的姿态和轨道控制系统的设计，实施和轨道展示
5. The design, implementation and testing of the thermal control system of the CanX-2 nanosatellite, and, The preliminary design of the attitude determination and control system for the generic nanosatellite bus. [D] . Sarda, Karan. 2006

机译：CanX-2纳米卫星热控制系统的设计，实施和测试，以及通用纳米卫星总线的姿态确定和控制系统的初步设计。
6. Quasi-All-Passive Thermal Control System Design and On-Orbit Validation of Luojia 1-01 Satellite [O] . Lin Yang, Qiang Li, Lin Kong, 2019

机译：罗家1-01卫星准全被动热控系统设计和在轨验证
7. Integrated Orbit, Attitude, and Structural Control System Design for Space Solar Power Satellites [O] . Moore Chris, Wie Bong, Roithmayr Carlos, 2001

机译：空间太阳能卫星的综合轨道，姿态和结构控制系统设计
8. Conceptual study of a micrometeoroid deep space satellite. volume iii- orbital mechan- ics, power supply and distribution, vehicle design, thermal control, attitude sensing and determination final report [R] . Pragluski, W. J., et al. 1965

机译：微流星体深空卫星的概念研究。体积三轨机械，供电和配电，车辆设计，热控制，姿态传感和确定最终报告

System Techniques, Satellites, Orbit Design, Thermal Control, Power Supply, Attitude Control, Telemetry System

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