介绍了气动中心高速所为航空航天飞行器所开展的动导数试验技术研究,主要包括高速大攻角动导数试验技术、再入体模型配平状态动导数试验技术及基于气体轴承的高超声速风洞模型滚转阻尼导数试验技术。阐述了这些试验技术的试验设备及测试系统,给出了典型的试验结果,并进行了分析与讨论 This paper introduces the research of dynamic derivative test technology for aerospace vehicle at high speed aerodynamic center, which mainly includes high speed large angle of attack derivative test technology, kinetic derivative test of reentry body model and hypersonic wind tunnel model based on gas bearing Rolling Damping Derivative Test Technique. The test equipment and test system of these test technologies are expounded, the typical test results are given and analyzed and discussed