← Search

Luke Soe Thura Win

7 accepted papers

2026

A Data-Driven Approach for Control and Stabilization of a Single Actuator Monocopter

ICRA 2026poster

In this paper, we use a machine learning approach to stabilize a Single Actuator Monocopter (SAM), showing its ability to operate autonomously outdoors utilizing an onboard Inertial Measurement Unit (IMU). We introduce a neural network-based proportional stabilizer that works in parallel to cascaded…

Cited by 0Scholar
2026

Wind-Aware Aerial Deployment and Control Strategy for Precision Landing of Single-Actuator Autorotating Wing

ICRA 2026poster

The Samara Autorotating Wing (SAW) is a bioinspired autorotating glider capable of both controlled autorotation and diving modes. This work presents control and deployment strategies that enable precision landing of the platform from low altitude. The proposed control approach leverages cyclic contr…

Cited by 0Scholar
2023

A Self-Rotary Aerial Robot With Passive Compliant Variable-Pitch Wings

RA-L 2023

Inspired by maple seeds, the self-rotary winged aerial robots reflect the advantages of both multi-rotor aircraft and fixed-wing robots. However, their self-rotating speed is related to the takeoff weight, which may affect their application and flight stabilization. To provide a practical and feasib

Cited by 4SourceScholar
2022

Cooperative Modular Single Actuator Monocopters Capable of Controlled Passive Separation

ICRA 2022poster

In this paper, we introduce a Modular Single Actuator Monocopter (M-SAM), which is capable of flying in both singular configuration and cooperative configuration. From singular mode, M-SAMs can be manually assembled into cooperative mode, using magnetic connectors built into the body of each M-SAM u…

Cited by 12SourceScholar
2021

Joint Mechanical Design and Flight Control Optimization of a Nature-Inspired Unmanned Aerial Vehicle via Collaborative Co-Evolution

RA-L 2021

In this work, a collaborative co-evolution approach is adopted to solve a joint physical design and feedback control optimization problem of a nature-inspired Unmanned Aerial Vehicle (UAV). Unlike traditional multirotors and fixed-wing aircraft, lift is achieved by spinning its entire body with atta

Cited by 8SourceScholar
2019

Dynamics and Control of a Collaborative and Separating Descent of Samara Autorotating Wings

RA-L 2019

To deliver lightweight sensor payloads to disaster-struck areas by means of an aerial deployment, a novel bio-inspired method capitalizing on autorotation to slow down vertical descent rate is proposed. This concept is illustrated using the samara autorotating wing (SAW) platform, which features a u

Cited by 19SourceScholar
2017

Orientation filter and angular rates estimation in monocopter using accelerometers and magnetometer with the Extended Kalman Filter

ICRA 2017poster

In monocopter flight, two important parameters are required for control: angular rates and heading direction. Small monocopters fly at a very high speed (more than 600rpm), which can be out of the typical gyroscope limit. Very high speed gyroscopes do exist, but the price is high and it can only mea…

Cited by 13SourceScholar