High angle of attack approach and landing control law design for the X-31A-Reference-Cited by-同舟云学术

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High angle of attack approach and landing control law design for the X-31A

Published:2002-01-14 Issue: Volume: Page:
ISSN:
Container-title:40th AIAA Aerospace Sciences Meeting & Exhibit
language:
Short-container-title:

Author:

Beh H.¹,Fischer B.,van den Bunt R.

Affiliation:

1. European Aeronautic Defense and Space Co., Munich, Germany

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-247

Reference7 articles.

1. Autonomous Landing Using the X-31A Aircraft, AIAA GNCConference 2001

2. 1 m) 43.2ft (13.2m) Figure 1:Configuration of theX-31A

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1. Assessment of the possibility of shortening the landing distance of maneuverable aircraft;VESTNIK of Samara University. Aerospace and Mechanical Engineering;2023-11-03

2. Information Fusion-Based Optimal Attitude Control for an Alterable Thrust Direction Unmanned Aerial Vehicle;International Journal of Advanced Robotic Systems;2013-01-01

3. Anti-crosswind Autolanding of UAVs based on Active Disturbance Rejection Control;AIAA Guidance, Navigation, and Control Conference;2010-06-26

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