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Attitude projection method for analyzing large-amplitude airplane maneuvers

  • Published:1990-01 Issue:1 Volume:13 Page:22-29
  • ISSN:0731-5090
  • Container-title:Journal of Guidance, Control, and Dynamics
  • language:en
  • Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Kato Osamu1

Affiliation:

1. Nagoya University, Nagoya, Japan

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

Cited by 13 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. Automated Generation of Realistic Near-Optimal Aircraft Trajectories;Journal of Guidance, Control, and Dynamics;2008-05

2. Automated Solution of Realistic Near-Optimal Aircraft Trajectories Using Computational Optimal Control and Inverse Simulation;AIAA Guidance, Navigation and Control Conference and Exhibit;2007-06-15

3. Trajectory generation for transition from VTOL to wing-borne flight using inverse dynamics;38th Aerospace Sciences Meeting and Exhibit;2000-01-10

4. Flying is solving inverse problems from the pilot's point of view;21st Atmospheric Flight Mechanics Conference;1996-07-29

5. Inverse and optimal control for precision aerobatic maneuvers;Journal of Guidance, Control, and Dynamics;1996-03
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