Quadrotor Precision Landing on Inclined Surfaces Using Adaptive Leg Design with Robust PID and Fractional PID Control

This work introduces a new system with adaptive landing legs to improve the versatility of quadrotor aerial platforms, facilitating safe take-off and landing on sloping surfaces. The design has a lightweight, symmetric leg construction powered by a single servomotor, reducing weight and streamlining wiring, while ensuring stability and balance in flight. To achieve accurate landings on slopes, essential data—including distance, slope orientation, and surface angle—is collected by a multi-zone Time-of-Flight sensor, which demonstrates resilience to visual distortions and fluctuating lighting conditions, surpassing conventional imaging techniques. Landing manoeuvre control is refined using MATLAB simulations, whereby we implement and compare proportional-integral-derivative (PID) and fractional-order PID controllers, emphasising the superior stability and precision of our control methodology. This design markedly enhances the manoeuvrability of quadrotors in difficult terrains.

Authors

Institutions

Publication Details

Published
2025-02-07
DOI
https://doi.org/10.1109/cspa64953.2025.10933327
Primary Topic
Hydraulic and Pneumatic Systems
Type
article
Field-Weighted Citation Impact
0.00
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

Quadrotor Precision Landing on Inclined Surfaces Using Adaptive Leg Design with Robust PID and Fractional PID Control

Ghulam E Mustafa Abro, Ayman M. Abdallah, Abdullah Nader Alkhater
Hydraulic and Pneumatic Systems
article

Quadrotor Precision Landing on Inclined Surfaces Using Adaptive Leg Design with Robust PID and Fractional PID Control

Ghulam E Mustafa Abro, Ayman M. Abdallah, Abdullah Nader Alkhater
article en

Abstract

This work introduces a new system with adaptive landing legs to improve the versatility of quadrotor aerial platforms, facilitating safe take-off and landing on sloping surfaces. The design has a lightweight, symmetric leg construction powered by a single servomotor, reducing weight and streamlining wiring, while ensuring stability and balance in flight. To achieve accurate landings on slopes, essential data—including distance, slope orientation, and surface angle—is collected by a multi-zone Time-of-Flight sensor, which demonstrates resilience to visual distortions and fluctuating lighting conditions, surpassing conventional imaging techniques. Landing manoeuvre control is refined using MATLAB simulations, whereby we implement and compare proportional-integral-derivative (PID) and fractional-order PID controllers, emphasising the superior stability and precision of our control methodology. This design markedly enhances the manoeuvrability of quadrotors in difficult terrains.

King Fahd University of Petroleum and Minerals (SA)
Affordable and clean energy
Openalex Percentile: Top 95%
Hydraulic and Pneumatic 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.

Quadrotor Precision Landing on Inclined Surfaces Using Adaptive Leg Design with Robust PID and Fractional PID Control — Ghulam E Mustafa Abro, Ayman M. Abdallah, et al. · (2025) | TGRS Research Map | TGRS