Altitude Control for Small Fixed-Wing Aircraft Using H∞ Loop-Shaping Method-Reference-Cited by-同舟云学术

Altitude Control for Small Fixed-Wing Aircraft Using H∞ Loop-Shaping Method

Published:2016 Issue:9 Volume:49 Page:111-116
ISSN:2405-8963
Container-title:IFAC-PapersOnLine
language:en
Short-container-title:IFAC-PapersOnLine

Author:

Akyurek Seyma,Kaynak Unver,Kasnakoglu Cosku

Publisher

Elsevier BV

Subject

Control and Systems Engineering

Reference19 articles.

1. Efe, M.Ö. (2007), Robust Low Altitude Behaviour Control of a Quadrotor Rotorcraft through Sliding Modes, Mediterranean Conference on Control and Automation

2. Kojima, R., Ogawara, K., Yoneda, T., Tomoigawa, S., (2008) Delayed Feedback Altitude Control for Micro UAV without Sensing Pitch Rate, International Conference on Control, Automation and Sytems, 316-319

3. Akyurek, S. (2015), Modelling and Loop-Shaping Control Design for Fixed-Wing Unmanned Aerial Vehicles

4. Young, C. M., Lynch, E.E., Boynton, E.R. (1944), Electrical Control in Automatic Pilots, Electrical Engineering IEEE, Volume 63, Issue 12, pp 939

5. Litchford, G.B., Tatz, A., Battle, F.H. Jr. (1959), A Look at the Future of Automatic Landing Systems, IRE Transactions on Aeronautical and Navigational Electronics, 118-128

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