Modeling and Design Considerations for Robust Control of Aircraft in Tight Cruise Formation-Reference-Cited by-同舟云学术

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Modeling and Design Considerations for Robust Control of Aircraft in Tight Cruise Formation

Published:2013-08-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control (GNC) Conference
language:
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Author:

Kienitz Karl H.¹,Kaden André²,Luckner Robert²

Affiliation:

1. Technological Institute of Aeronautics (ITA)

2. Technical University of Berlin

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-4858

Reference20 articles.

1. Beukenberg, M. "Beiträge zu Aerodynamik und Flugmechanik des Formationsfluges, " Doctoral Dissertation,Technische Universität Braunschweig, Germany, 1989.

2. Formation Flight Optimization Using Extremum Seeking Feedback

3. Design and flight-testing of non-linear formation control laws

4. Peak-Seeking Control for Drag Reduction in Formation Flight

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1. Maneuvers During Automatic Formation Flight of Transport Aircraft for Fuel Savings;Journal of Aircraft;2021-11-11

2. Maneuvers during Automatic Formation Flight of Transport Aircraft for Fuel Savings;AIAA Scitech 2020 Forum;2020-01-05

3. Flight Control Systems for fuel efficient wake surfing;AIAA Scitech 2020 Forum;2020-01-05

4. Dynamic Load Alleviation in Wake Vortex Encounters;Journal of Guidance, Control, and Dynamics;2016-04

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