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《Flight Dynamics》 2008-01
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Recent Status and Development Review of Spacecraft Reentry Guidance Methods

CHEN Gang1,2,DONG Long-lei1,YAN Gui-rong1,XU Min2,CHEN Shi-lu2(1.College of Astronautics and Aeronautics,Xi'an Jiaotong University,Xi'an 710049,China;2.College of Astronautics,Northwestern Polytecnical University,Xi'an 710072,China)  
This paper introduce the recent development of the spacecraft reentry guidance method in the world.According to the reference trajectory guidance law and predictor-corrector guidance law,it analyzes the framework and design idea of these new guidance laws in detail.Finally we indicate that the autonomous,adaptive and robust reentry guidance law with multi-task flexibility is the focus and direction in the field.
【Fund】: 国家863计划资助项目(2006AA0978)
【CateGory Index】: V448.2
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