Path following control for quadcopters with super twisting sliding mode control with PID sliding surface technique

This article proposes a novel super twisting sliding mode control with PID sliding surface (PID-STSMC) to improve path following and hovering maneuvers of the quadcopter. The proposed controller is robust as it ensures that the quadcopter track the desired path with a very small error and minimum control effort even in the presence of the periodic disturbances, sensor noise, and wind disturbances. The simulation results conform the effectiveness of the proposed controller in path following and hovering maneuvers of the quadcopter. The proposed controller outperforms the existing controller, proportional integral derivative sliding mode control, and proportional integral derivative adaptive sliding mode control when compared.

Authors

Institutions

Publication Details

Journal
Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering
Published
2025-09-25
DOI
https://doi.org/10.1177/09544100251381422
Primary Topic
Adaptive Control of Nonlinear Systems
Type
article
Field-Weighted Citation Impact
0.00
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

Path following control for quadcopters with super twisting sliding mode control with PID sliding surface technique

Sanjay Kumar, Lillie Dewan
Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering
Adaptive Control of Nonlinear Systems
article

Path following control for quadcopters with super twisting sliding mode control with PID sliding surface technique

Sanjay Kumar, Lillie Dewan
article en

Abstract

This article proposes a novel super twisting sliding mode control with PID sliding surface (PID-STSMC) to improve path following and hovering maneuvers of the quadcopter. The proposed controller is robust as it ensures that the quadcopter track the desired path with a very small error and minimum control effort even in the presence of the periodic disturbances, sensor noise, and wind disturbances. The simulation results conform the effectiveness of the proposed controller in path following and hovering maneuvers of the quadcopter. The proposed controller outperforms the existing controller, proportional integral derivative sliding mode control, and proportional integral derivative adaptive sliding mode control when compared.

Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace EngineeringVol. 240(3)
National Institute of Technology Kurukshetra (IN)
Openalex Percentile: Top 67%
Adaptive Control of Nonlinear Systems
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.