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State Variance-Based Approach to Flight Dynamic Constraints in Multidisciplinary Design Optimization

  • Published:2017-05 Issue:5 Volume:40 Page:1206-1220
  • ISSN:0731-5090
  • Container-title:Journal of Guidance, Control, and Dynamics
  • language:en
  • Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Morris Craig C.1,Sultan Cornel1,Schetz Joseph A.1,Kapania Rakesh K.1

Affiliation:

1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061

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

Reference32 articles.

1. “Flying Qualities of Piloted Aircraft,” U.S. Dept. of Defense, Dept. of Defense Interface STD MIL-STD-1797A, Feb. 1990.

2. CooperG. E.HarperR. P. “The Use of Pilot Rating in the Evaluation of Aircraft Handling Qualities,” NASA TN D-5153, April 1969.

3. The Evolution, Revolution, and Challenges of Handling Qualities

4. GilruthR. R. “Requirements for Satisfactory Flying Qualities of Airplanes,” NACA TR 755, 1943.

5. “Flying Qualities of Piloted Airplanes,” U.S. Air Force MIL-SPEC MIL-F-8785A, Nov. 1968.

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Design Methodology of a Mini-Missile Considering Flight Performance and Guidance Precision;Journal of Systems Engineering and Electronics;2024-02

2. A model‐based flight qualities evaluation approach for civil aircraft;Concurrency and Computation: Practice and Experience;2018-10-02
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