Pitch Control Law Analysis and Flight Test Demonstration of an Executive Transport Aircraft-Reference-Cited by-同舟云学术

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Pitch Control Law Analysis and Flight Test Demonstration of an Executive Transport Aircraft

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
language:
Short-container-title:

Author:

Shin Jong-Yeob¹,Harden Clay¹,Saeed Nomaan¹,Hartley Robert¹,Chen Kaiming¹

Affiliation:

1. Gulfstream Aerospace Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-6120

Reference15 articles.

1. A Course in Robust Control Theory

2. Boyd, S., Ghaoui, L.E., Feron, E. and Balakrishnan, V. "Linear Matrix Inequalities in System and Control Theory", SAIMStudiesinAppliedmathematics,1994.

3. Gahinet,P.,Nemirouski,A.,Laub,A.J.,andChilai,M,"LMI ControlToolbox",TheMathworks,1995.

Cited by 3 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 of a Pitch Axis Autopilot Control Law for an Executive Transport Aircraft;AIAA Scitech 2019 Forum;2019-01-06

2. Closed Loop Control Law Stability and Performance Analysis Directly Using Open Loop Flight Test Data;AIAA Guidance, Navigation, and Control Conference;2012-08-13

3. Robustness Analysis on Pitch Control Law for an Executive Transport Aircraft;AIAA Guidance, Navigation, and Control Conference;2010-06-26

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