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Jun En Low

6 accepted papers

2025

SOUS VIDE: Cooking Visual Drone Navigation Policies in a Gaussian Splatting Vacuum

RA-L 2025

We propose a new simulator, training approach, and policy architecture, collectively called SOUS VIDE, for end-to-end visual drone navigation. Our trained policies exhibit zero-shot sim-to-real transfer with robust real-world performance using only onboard perception and computation. Our simulator,

Cited by 18SourceScholar
2022

Aerial Grasping and the Velocity Sufficiency Region

RA-L 2022

A largely untapped potential for aerial robots is to capture airborne targets in flight. We present an approach in which a simple dynamic model of a quadrotor/target interaction leads to the design of a gripper and associated velocity sufficiency region with a high probability of capture. A model of

Cited by 30SourceScholar
2018

Direction Controlled Descent of Samara Autorotating Wings (SAW) with N-Wings

ICRA 2018poster

The seeds of Maple trees (Samara) use autorotation as a unique mechanism to disperse their seeds. By exploiting gyroscopic stability of a spinning wing, the Samara is able to cover large horizontal distance despite having no form of propulsion. We applied and adapted this natural ability in our nove…

Cited by 15SourceScholar
2018

Direction Controlled Descent of Samara Autorotating Wings (SAW) with N-Wings * Research supported by the SUTD-MIT International Design Centre (IDC) and by the Temasek Laboratories Defence Innovation Research Programme (DIRP) IGDSP15020141

ICRA 2018

The seeds of Maple trees (Samara) use autorotation as a unique mechanism to disperse their seeds. By exploiting gyroscopic stability of a spinning wing, the Samara is able to cover large horizontal distance despite having no form of propulsion. We applied and adapted this natural ability in our nove

Cited by 27SourceScholar
2017

Design and dynamic analysis of a Transformable Hovering Rotorcraft (THOR)

ICRA 2017poster

This paper describes the Transformable HOvering Rotorcraft (THOR), a prototype Unmanned Aerial Vehicle (UAV) that explores a novel approach in combining the range and speed of a horizontal flying platform with the hovering and maneuverability of a rotor-wing. This is achieved by integrating a taille…

Cited by 52SourceScholar
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