作者: M. Aznar Fernandez-Montesinos , G. Schram , R. A. Vingerhoeds , H. B. Verbruggen , J. A. Mulder
DOI: 10.2514/2.7624
关键词:
摘要: Many aircraft accidents are related to hazardous windshear phenomena, in particular the microburst. The energy loss which is associated with a microburst encounter can be very dangerous for at low altitude. In this paper, recovery concept introduced, making distinction between control, guidance, and flight envelope protection. For fuzzy logic controller developed based on principles, since basically an problem. Additional automatically supplied during by increasing thrust. available distributed altitude airspeed pitch angle according priority assignment, activated of windshear. This determined respect minimum altitude, protection mechanism. Both integrated one system. Once bounds guaranteed, tracks path indicated predetermined guidance strategy. application demonstrated realistic simulation example.