An In-Flight Investigation to Develop Control System Design Criteria for Fighter Airplanes. Volume 2. Appendices 1 through 5-Reference-Cited by-同舟云学术

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An In-Flight Investigation to Develop Control System Design Criteria for Fighter Airplanes. Volume 2. Appendices 1 through 5

Published:1970-12-01 Issue: Volume: Page:
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Author:

Neal T. P.,Smith Rogers E.

Publisher

Defense Technical Information Center

Cited by 6 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. Review on Flight Control Law Technologies of Fighter Jets for Flying Qualities;International Journal of Aeronautical and Space Sciences;2022-12-31

2. Adaptive Incremental Nonlinear Dynamic Inversion Flight Control for Consistent Handling Qualities;AIAA SCITECH 2022 Forum;2022-01-03

3. Assessment of a Scalogram-Based Pilot-Induced Oscillation Metric with Flight-Test and Simulation Data;Journal of Guidance, Control, and Dynamics;2020-11

4. Pilot-in-the-Loop Analysis of Aileron Operation and Flight Simulator Experiments;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2007

5. Controller Design Using Standard Pilot Model;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2003

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