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Hauptverfasser: Srivastava, Astik, Indu, S., Sharma, Richa
Format: Preprint
Veröffentlicht: 2024
Schlagworte:
Online-Zugang:https://arxiv.org/abs/2404.12261
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author Srivastava, Astik
Indu, S.
Sharma, Richa
author_facet Srivastava, Astik
Indu, S.
Sharma, Richa
contents This paper presents the design, implementation, and flight test results of linear quadratic integral regulator (LQRi) based attitude control for a quadcopter UAV. We present the derivation of the mathematical model for the kinematics and dynamics of the UAV, along with the linearized state space representation of the system about hover conditions. LQR and LQRi controllers are then designed to stabilize the UAV in hover conditions and to track desired attitude commands. The controllers are then implemented onboard the Pixhawk flight controller and flight test results are discussed. Finally, the code related to this paper has been published open-source for replication and further research
format Preprint
id arxiv_https___arxiv_org_abs_2404_12261
institution arXiv
publishDate 2024
record_format arxiv
spellingShingle Design And Flight Testing Of LQRi Attitude Control For Quadcopter UAV
Srivastava, Astik
Indu, S.
Sharma, Richa
Robotics
This paper presents the design, implementation, and flight test results of linear quadratic integral regulator (LQRi) based attitude control for a quadcopter UAV. We present the derivation of the mathematical model for the kinematics and dynamics of the UAV, along with the linearized state space representation of the system about hover conditions. LQR and LQRi controllers are then designed to stabilize the UAV in hover conditions and to track desired attitude commands. The controllers are then implemented onboard the Pixhawk flight controller and flight test results are discussed. Finally, the code related to this paper has been published open-source for replication and further research
title Design And Flight Testing Of LQRi Attitude Control For Quadcopter UAV
topic Robotics
url https://arxiv.org/abs/2404.12261