航天器轨道动力学是航天工程的基础。 轨道设计、轨道确定、轨道控制、轨道拦截、交会对接、编队飞行和再入返回等技术问题都需要以轨道动力学理论为基础。本书适合从事航天器研究、设计、试验和应用的科技工作者和航空宇航科学与技术学科研究生、高年级本科生阅读。Orbital dynamics of spacecraft is the basis of aerospace engineering. Orbit design， orbit determination， orbitcontrol， orbital intercept， rendezvous and docking， formation flight and re-entry and other technical issues need toreturn to the track dynamics based on the theory.This book are suitable for spacecraft research， design， testing and application of scientific and technologicalworkers and aviation aerospace science and technology disciplines graduate students， senior undergraduates to read.