Range maximization for emergency landing after engine cutoff

Journal of Aircraft

Volumn 42, Issue 5, 2005, Pages 1296-1306

  Shapira, Ilana ^a,b   Ben Asher, Joseph ^a,c  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

^b Faculty of Aeronautical Engineering   (Israel)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRCRAFT LANDING; BOUNDARY LAYERS; OPTIMIZATION;

DYNAMIC PHASE; QUASI-STEADY-STATE GLIDE; SAFE LANDING;

ALGORITHMS;

EID: 27144522272     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.10042     Document Type: Article

References (6)

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3. Rao, A. V., and Mease, K. D., "Eigenvector Approximate Dichotomic Basis Method for Solving Hyper-Sensitive Optimal Control Problems," Optimal Control Applications and Methods, Vol. 21, No. 1, 2000, pp. 1-19.
4. Ardema, M. D., and Rajan, N., "Separation of Time Scales in Aircraft Trajectory Optimization," Journal of Guidance, Control, and Dynamics, Vol. 8, No. 2, 1985, pp. 275-278.
5. Shapira, I., and Ben-Asher, J. Z., "Singular Perturbation Analysis of Optimal Glide," Proceeding of the AIAA/AFM Conference, Aug. 2002.
6. Shapira, I., and Ben-Asher, J. Z., "Singular Perturbation Analysis of Optimal Glide" Journal of Guidance, Control, and Dynamics, Vol. 27, No. 5, 2004, pp. 915-918.