Appendix B: Summary of Orbital Mechanics Relevant to Remote Sensing

C. Elachi, J. V. Zyl
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Abstract

Orbit selection and sensor characteristics are closely related to the strategy required to achieve the desired results. Different types of orbits are required to achieve continuous monitoring, repetitive coverage of different periodicities, global mapping, or selective imaging. The vast majority of earth-orbiting remote sensing satellites use circular orbits. Planetary orbiters usually have elliptical orbits, which are less taxing on the spacecraft orbital propulsion system and combine some of the benefits of high and low orbits thus allowing a broader flexibility to achieve multiple scientific objectives.
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附录B:与遥感有关的轨道力学摘要
轨道选择和传感器特性与实现预期结果所需的策略密切相关。需要不同类型的轨道来实现连续监测、不同周期的重复覆盖、全球制图或选择性成像。绝大多数地球轨道遥感卫星使用圆形轨道。行星轨道飞行器通常有椭圆轨道,这对航天器轨道推进系统的负担较小,并且结合了高轨道和低轨道的一些好处,从而允许更大的灵活性来实现多个科学目标。
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Appendix D: Compression of a Linear FM Chirp Signal Appendix A: Use of Multiple Sensors for Surface Observations Atmospheric Remote Sensing in the Microwave Region Nature and Properties of Electromagnetic Waves Appendix B: Summary of Orbital Mechanics Relevant to Remote Sensing
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