Piloted Simulator Evaluation Results of Flight Physics Based Stall Recovery Guidance

Lombaerts, Thomas ; Schuet, Stefan ; Stepanyan, Vahram ; Kaneshige, John ; Hardy, Gordon ; Shish, Kimberlee ; Robinson, Peter

关键词: VERTICAL MOTION SIMULATORS;    AERODYNAMIC STALLING;    ALGORITHMS;    TEST PILOTS;    FLIGHT CONTROL;    SIMULATORS;    CONTROLLABILITY;    PILOT PERFORMANCE;    PILOT TRAINING;    PREDICTIONS;    MALFUNCTIONS;    CIVIL AVIATION;   

RP-ID  :  ARC-E-DAA-TN50867

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

In recent studies, it has been observed that loss of control in flight is the most frequent primary cause of accidents. A significant share of accidents in this category can be remedied by upset prevention if possible, and by upset recovery if necessary, in this order of priorities. One of the most important upsets to be recovered from is stall. Recent accidents have shown that a correct stall recovery maneuver remains a big challenge in civil aviation, partly due to a lack of pilot training. A possible strategy to support the flight crew in this demanding context is calculating a recovery guidance signal, and showing this signal in an intuitive way on one of the cockpit displays, for example by means of the flight director. Different methods for calculating the recovery signal, one based on fast model predictive control and another using an energy based approach, have been evaluated in four relevant operational scenarios by experienced commercial as well as test pilots in the Vertical Motion Simulator at NASA Ames Research Center. Evaluation results show that this approach could be able to assist the pilots in executing a correct stall recovery maneuver.