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An H∞ Design Approach for the Heading Hold Autopilot of a Flying Wing UAV

Year: 2016

Type: article

Abstract: The paper presents a modified loop shaping approach for the design of the automatic flight control system of an unmanned air vehicle’s lateral-directional dynamics. The design objectives include robust stabilization with respect to modeling uncertainties, heading angle tracking of an ideal model, coordinated turn and reduced sensitivity with respect to low frequency measurement errors. Based on the resulting full order controller one determined a reduced order controller. The numerical results show that both the full order and the reduced order autopilots accomplish the design objectives.

Source: Applied Mechanics and Materials

DOI: 10.4028/www.scientific.net/amm.841.315

Authors: Adrian Mihail Stoica, Petrişor Valentin Parvu, Mirela Bivolaru

Institution: Universitatea Națională de Știință și Tehnologie Politehnica București

Language: English

Topic: Aerospace Engineering and Control Systems

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: hybrid

OpenAlex ID: W2467989282

FWCI: 0.389

Cites:

Cited by: 1

Related to: 10