Time-Optimal Path Following for Fixed-Wing Aircraft-Reference-Cited by-同舟云学术

Time-Optimal Path Following for Fixed-Wing Aircraft

Published:2013-01 Issue:1 Volume:36 Page:83-95
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Zhao Yiming¹,Tsiotras Panagiotis²

Affiliation:

1. Mitsubishi Electric Research Laboratories, Cambridge, Massachusetts 02139

2. School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332-0150

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.57471

Reference17 articles.

1. Inverse dynamics approach to trajectory optimization for an aerospace plane

2. Application of Direct Transcription to Commercial Aircraft Trajectory Optimization

3. Airspace Constraints in Aircraft Emission Trajectory Optimization

4. ZhaoY. “Efficient and Robust Aircraft Landing Trajectory Optimization,” Ph.D. Thesis, School of Aerospace Engineering, Georgia Inst. of Technology, Atlanta, 2011.

5. NilssonN. J., Principles of Artificial Intelligence, Tioga Publ., Palo Alto, CA, 1980, pp. 77–78.

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