Robust Nonlinear Non-Referenced Inertial Frame Multi-Stage PID Controller for Symmetrical Structured UAV
The design and implementation of a multi-stage PID (MS-PID) controller for non-inertial referenced UAVs are highly complex. Symmetrical multirotor UAVs are unstable systems, and it is thought that the kinematics of the symmetrical UAV rotor, such as the quadrotor and hexacopter resembles the kinemat...
Main Authors: | Ajlouni, F. (Author), Ajlouni, N. (Author), Al Kasasbah, B. (Author), Alshahrani, A. (Author), Özyavaş, A. (Author), Takaoğlu, F. (Author) |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI
2022
|
Subjects: | |
Online Access: | View Fulltext in Publisher |
Similar Items
-
Purwarupa Sistem Kendali Kestabilan Pesawat Tanpa Awak Sayap Tetap Menggunakan Robust PID
by: Dwitiya Bagus Widyantara, et al.
Published: (2016-10-01) -
PID Controller Design for Cruise Control System using Particle Swarm Optimization
by: Ahmed Abdulnabi
Published: (2017-12-01) -
Fuzzy adaptive PID control for six rotor eppo UAV
by: Yongwei LI, et al.
Published: (2017-02-01) -
Computer aided synthesis and design of PID controllers
by: Mitra, Sandipan
Published: (2008) -
Computer aided synthesis and design of PID controllers
by: Mitra, Sandipan
Published: (2010)