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Piloted Simulator Evaluation Results of Flight Physics Based Stall Recovery Guidance
Author(s) -
Thomas Lombaerts,
Stefan Schuet,
Vahram Stepanyan,
John Kaneshige,
G. H. Hardy,
Kimberlee H. Shish,
Peter Robinson
Publication year - 2018
Publication title -
aiaa guidance, navigation and control conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2018-0383
Subject(s) - flight simulator , simulation , computer science , stall (fluid mechanics) , aerospace engineering , aeronautics , physics , engineering
Recent studies have shown 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 recover 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 supports the pilots in improving their stall recovery performance.

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