Application of H 2 /H ∞ and dynamic inversion techniques to aircraft landing control

Title
Application of H 2 /H ∞ and dynamic inversion techniques to aircraft landing control
Authors
Keywords
Aircraft landing, control, Dynamic inversion, Glide slope, Flare
Journal
AEROSPACE SCIENCE AND TECHNOLOGY
Volume 46, Issue -, Pages 146-158
Publisher
Elsevier BV
Online
2015-07-18
DOI
10.1016/j.ast.2015.07.005

Ask authors/readers for more resources

Reprint

Contact the author

Create your own webinar

Interested in hosting your own webinar? Check the schedule and propose your idea to the Peeref Content Team.

Create Now

Ask a Question. Answer a Question.

Quickly pose questions to the entire community. Debate answers and get clarity on the most important issues facing researchers.

Get Started