Conference proceedings | ©2022
Proceedings of ALL WORLD MUSLIM EDUCATIONAL CONFERENCE (AWMEC’22) PROCEEDINGS
Comparison Between the Various Optimal Trajectories in (3-D) and Their Effect on Control Effort of a Quadrotor UAV
Abstract
In this work, Newton’s land Euler’s law is used for the development and the study of the various trajectories of the quadrotor. This study discussed the four orbits of the quadrotor each of them is characterized as Snap, Jerk, Acceleration, and Velocity orbits. The linearized model of the unmanned aerial vehicles (UAV) is surveyed, and the results of the different orbital positions are examined. A proportional differential integral (PID) controller or a linear quadratic controller is designed for the study of the various orbital positions of the quadrotor. In the first part, the mathematical model is discussed which is used for the development of the model. The fundamental entity which is generally characterized as the degree of freedom and is abbreviated as the DOF is also discussed.
Keywords: Proportional differential integral, unmanned aerial vehicles, Degree of freedom, Trajectories
Keywords
Proportional differential integral, unmanned aerial vehicles, Degree of freedom, Trajectories
References
Mohsin, M. Y., Tahir, S., Yousif, M., Farid, G., Tahir, W., & Wattoo, W. A. (2022). Comparison Between the Various Optimal Trajectories in (3-D) and Their Effect on Control Effort of a Quadrotor UAV. In Proceedings of the All World Muslim Educational Conference (AWMEC’22) (p. 35). IJSmart Publishing.
Editors and Affiliations
Muhammad Yasin Mohsin1, Sohaib Tahir2, Muhammad Yousif3, Ghulam Farid4, Waqar Tahir5, Waqas Ahmad Wattoo6
- USPCAS-E National University of Sciences and Technology (NUST), Islamabad, Pakistan. Email:muhammadyasinmohsin806@gmail.com;
- Comsats University Islamabad Sahiwal Campus Pakistan; Email: sohaibtahir@cuisahiwal.edu.pk
- USPCAS-E National University of Sciences and Technology (NUST), Islamabad, Pakistan. Email: yousif@uspcase.nust.edu.pk
- Comsats University Islamabad Sahiwal Campus Pakistan. Email: gfarid@cuisahiwal.edu.pk
- Comsats University Islamabad Sahiwal Campus Pakistan. Email: waqarntahir@cuisahiwal.edu.pk
- Comsats University Islamabad Sahiwal Campus Pakistan. Email: waqqas@cuisahiwal.edu.pk
Copyright information
© 2022 IJSmart Publishing Company. All rights reserved. No part of this publication may be reproduced or distributed without permission.
About this paper
In the first part, the mathematical model is discussed which is used for the development of the model. The fundamental entity which is generally characterized as the degree of freedom and is abbreviated as the DOF is also discussed.