基于DGPS的非稳态条件下空速校准方法

准确的空速和高度是进行飞行试验和确保飞行安全的基础,最新的民用运输类飞机适航标准要求在飞机全包线范围内都要进行空速系统校准。飞机在地面滑跑阶段和失速过程中速度是急剧变化的,而传统的空速校准方法只适用于飞机稳定平飞的状态。介绍了DGPS综合法的原理,利用DGPS高度差与飞机压力高度差之间的关系,获得了非稳态条件下空速系统的位置误差结果,并成功应用于国产支线飞机的合格审定试验。 

Calibration Method of Airspeed Based on DGPS in Unsteady State

Accurate airspeed and altitude are the basis for flight testing and ensuring flight safety. The latest airworthiness standard for civil transport airplane requires airspeed system should be calibrated in the full envelope of the airplane. The speed of the airplane on the ground roll stage and stall process is rapidly changing, and traditional airspeed calibration method is only applicable for stable state. This paper introduces the principle of DGPS method, using the relationship between DGPS height difference and the pressure height difference, to obtain the results of airspeed system position error under non steady state conditions. And this method has successfully applied on domestic regional airplane flight tests.