作者: Sandeep S. Mulgund , Robert F. Stengel
DOI: 10.2514/3.21121
关键词: Engineering 、 Trajectory optimization 、 Airspeed 、 Stall (fluid mechanics) 、 Rate of climb 、 Microburst 、 Aerospace engineering 、 Flight control surfaces 、 Wind shear 、 Elevator
摘要: The flight path of a twin-jet transport aircraft is optimized in microburst encounter during approach to landing. objective execute an escape maneuver that maintains safe ground clearance and adequate stall margin the climb-out portion trajectory. A cost function penalizing rate climb deviations from nominal value elevator deflection produces qualitatively good results variety encounters. optimal gradual pitch-up ceases near core microburst, followed by slight reduction pitch attitude tailwind area microburst. minimum airs eed constraint optimization prevents excessive airspeed loss very severe microbursts. #' he equations motion include short-period dynamics, so solves directly for control surface deflections required achieve paths.