In this paper an uncertain norm-bounded mathematical model for the UAV HighAltitude Performance Demonstrator (HAPD) designed by Italian Aerospace ResearchCenter (CIRA) is carried out. The linear state space description aims todescribe the non-linear aircraft dynamic inside the operating envelopecharacterized by the following bounds: true air speed between 17 m/s and 23 m/sand altitude from 300 m to 700 m.

HAPD aircraft Uncertain Norm-Bounded Mathematical model

Valerio Scordamaglia
2019-01-01

Abstract

In this paper an uncertain norm-bounded mathematical model for the UAV HighAltitude Performance Demonstrator (HAPD) designed by Italian Aerospace ResearchCenter (CIRA) is carried out. The linear state space description aims todescribe the non-linear aircraft dynamic inside the operating envelopecharacterized by the following bounds: true air speed between 17 m/s and 23 m/sand altitude from 300 m to 700 m.
cs.SY
cs.SY
Mathematics - Dynamical Systems
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.12318/80350
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