Quaternion Attitude Control System of Highly Maneuverable Aircraft
In the era of rapid advancements in manned and unmanned aviation and robotics, there is a need for high-performance, robust attitude control of highly maneuverable fixed-wing aircraft, both manned and unmanned (UAVs). This paper presents an extension to research on spacecraft attitude control. The a...
Main Authors: | Michał Gołąbek, Michał Welcer, Cezary Szczepański, Mariusz Krawczyk, Albert Zajdel, Krystian Borodacz |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2022-11-01
|
Series: | Electronics |
Subjects: | |
Online Access: | https://www.mdpi.com/2079-9292/11/22/3775 |
Similar Items
-
A Unified Approach: Split Quaternions with Quaternion Coefficients and Quaternions with Dual Coefficients
by: Emel Karaca, et al.
Published: (2020-12-01) -
The Cubli: Modeling and Nonlinear Attitude Control Utilizing Quaternions
by: Fabio Bobrow, et al.
Published: (2021-01-01) -
An Improved Unit Quaternion for Attitude Alignment and Inverse Kinematic Solution of the Robot Arm Wrist
by: Abubaker Ahmed, et al.
Published: (2023-06-01) -
Research on the Update Method of Attitude Quaternion for Strapdown Inertial Navigation
by: Debiao Zhang, et al.
Published: (2021-01-01) -
Why and How to Avoid the Flipped Quaternion Multiplication
by: Hannes Sommer, et al.
Published: (2018-07-01)