Boeing/Sperry automatic landing system 727 airplane.

Parker, Richard H.; Templeman, J. E.

doi:10.2514/3.43940

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“…Classical design of FCS laws relies heavily on engineering skills and experience of the designers [2,3,4].There are also many modern control design methods to solve the multi-objective problem of autoland control. Some scholars adopted H∞, H2, LQG/LTR control technique to design autoland system encountering windshear [5,6], but researches above just focused on the theory, which do not fit the engineering requirements of CAT III landing.…”

Section: Introductionmentioning

confidence: 99%

CAT III Autoland Control Laws Design Based on Multi-Objective Optimization

Yang

Shen

2012

AMR

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The CAT III longitudinal automatic landing control laws based on multi-objective optimization is discussed. Firstly summarized the CAT III airworthiness criteria and transformed into the specifications of control system. The configuration of the longitudinal automatic landing controllers is proposed secondly and multi-objective optimization is used to tradeoff free parameters of the controllers. The Monte Carlo simulation results show the designed control laws fulfill the CAT III requirements, when there are uncertainties of structure, measurement error and disturbances.

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