NDLI: Research on the line stabilization law of the fresnel guiding glide slope

Content Provider	IEEE Xplore Digital Library
Author	Zhu Qidan Zhang Wen Wang Tong
Copyright Year	2009
Description	Author affiliation: College of Automatic, Harbin Engineering University, 150001, China (Zhu Qidan; Zhang Wen; Wang Tong)
Abstract	The Fresnel lens optical landing system (FLOLS) is the electro-optical pilot longitudinal landing aid for the carrier. The guiding principle and the stabilization theory of the FLOLS are analyzed here. The line stabilization strategy is analyzed, in order to build the line stabilization model, the transformation problem of the carrier rotational motion between different coordinate systems is solved, and then the guiding glide slope model basing on the line stabilization strategy is gained. At last the compensation effect of the line stabilization strategy is validated by the static simulation, and in order to study the motion lawof the line stabilization guiding glide slope, the dynamic simulation is done basing on the foreign carrier motion data. These researches provide the basis of the FLOLS control and practical applications.
Starting Page	3036
Ending Page	3041
File Size	754611
Page Count	6
File Format	PDF
ISBN	9781424427222
DOI	10.1109/CCDC.2009.5192852
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2009-06-17
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Europe Fresnel Lens Optical Landing System Educational institutions Aerospace control Azimuth Simulation Guiding Glide Slope Error correction Aircraft Motion analysis Assembly Monitoring Lenses Line Stabilization
Content Type	Text
Resource Type	Article

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Design and fabrication of Fresnel lenses

Total energy-rate feedback for automatic glide-slope tracking during wind-shear penetration

Flight-test of the glide-slope track and flare-control laws for an automatic landing system for a powered-lift stol airplane

Kinetic simulation research on the aircraft landing and arresting

Adaptive control of aircraft lateral directional axis using subspace stabilization

Guidance law simulation studies for complex approaches using the microwave landing system (mls)

The effect of landing system coverage and path geometry on lateral position errors at the runway threshold

Visual cueing aids for rotorcraft landings

Fuzzy controller design for automatic carrier landing of aircraft

Research on the line stabilization law of the fresnel guiding glide slope

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