| Mulgund, S.S, and Stengel, R.F., Optimal Recovery from Microburst Wind Shear, Journal of Guidance, Control, and Dynamics, Vol. 16, No. 6, pp. 1010-1017, 1993. |
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Mulgund, S.S., and Stengel, R.F. (1993b). "Optimal Recovery from Microburst Wind Shear," Journal of Guidance, Control, and Dynamics, Vol. 16, No. 6, pp. 1010- 1017.
....wind field knowledge. Because optimal trajectories cannot yet be generated in real time, OTA results are not immediately useful for aircraft control. Feedback control laws employing local wind field knowledge have thus been developed for near optimal flight control [13 15] In a recent paper [16] we presented an optimization study for jet transport encounters with microburst wind shear on final approach. The objective was to execute an escape maneuver that maintained safe ground clearance and an adequate stall margin during the climb out. A quadratic cost function penalizing deviations in ....
....appear linearly. The second element is differentiated twice as before. The resultant dynamics have the form T(t) h(t) v 6 v 7 (64) During an aborted landing maneuver, full throttle and a desired climb rate are commanded. Climb Rate Scheduling The trajectories developed in [16] show that an optimal guidance strategy during aborted landing maneuvers in wind shear is to schedule climb rate as a function of microburst strength: in weak to moderate microbursts, the aircraft smoothly shifts from a descent on the glide slope to an ascent at the target climb rate; in severe ....
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Mulgund, S.S., and Stengel, R.F., "Optimal Recovery from Microburst Wind Shear," J. of Guidance, Control, and Dynamics, Vol. 16, No. 6, Nov. - Dec. 1993.
No context found.
Mulgund, S.S, and Stengel, R.F., Optimal Recovery from Microburst Wind Shear, Journal of Guidance, Control, and Dynamics, Vol. 16, No. 6, pp. 1010-1017, 1993.
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