Automatic Take-Off and Landing of Tailwheel Aircraft with Incremental Nonlinear Dynamic Inversion-Reference-Cited by-同舟云学术

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Automatic Take-Off and Landing of Tailwheel Aircraft with Incremental Nonlinear Dynamic Inversion

Published:2022-01-03 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2022 Forum
language:
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Author:

Steinleitner Andreas¹,Frenzel Vincenz¹,Pfeifle Ole¹,Denzel Jan¹,Fichter Walter¹

Affiliation:

1. Universitat Stuttgart

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-1228

Reference20 articles.

1. MacDonald, A. F., and Peppler, I. L. Tricycle Versus Conventional Landing Gear, 22nded., Aviation Supplies & Academics, 1991, p.10.

2. Design of an autoland controller for an F-14 aircraft using H-infinity synthesis

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2. Robust Stability and Performance Analysis of Incremental Dynamic-Inversion-Based Flight Control Laws;Journal of Guidance, Control, and Dynamics;2023-09

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