论文信息 - Adaptive control of aircraft in windshear

Adaptive control of aircraft in windshear

The control of an aircraft encountering windshear after takeoff is treated as a problem of stabilizing the climb rate about a desired value. An adaptive strategy is developed which uses only climb rate information. Robustness vis-a-vis windshear structure and intensity is illustrated via simulations employing four different windshear models. Simulations were carried out for a Boeing-727 aircraft with three JT8D-17 turbofan engines.<<ETX>>

[1] Michael E. Long. The air-safety challenge , 1977 .

[2] Angelo Miele,et al. Guidance strategies for near-optimum take-off performance in a windshear , 1986 .

[3] R. L. Bowles,et al. Maximum survival capability of an aircraft in a severe windshear , 1987 .

[4] A. Miele,et al. Optimization and guidance of abort landing trajectories in a windshear , 1987 .

[5] R. L. Bowles,et al. Gamma guidance schemes for flight in a windshear , 1988 .

[6] Y. H. Chen,et al. Robust control strategy for take-off performance in a windshear , 1989 .

[7] Yiyuan Zhao,et al. Control of an aircraft in downbursts , 1990 .

[8] Walter J. Grantham,et al. DFW microburst model based on AA-539 data , 1990 .

[9] Yiyuan Zhao,et al. Optimal paths through downbursts , 1990 .

[10] George Leitmann,et al. Deterministic control of uncertain systems via a constructive use of Lyapunov stability theory , 1990 .

[11] George Leitmann,et al. Aircraft control for flight in an uncertain environment: Takeoff in windshear , 1991 .

[12] M. A. Zarkh,et al. Numerical solution of linear differential games , 1991 .