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Posts

Future Blog Post

less than 1 minute read

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This post will show up by default. To disable scheduling of future posts, edit config.yml and set future: false.

Blog Post number 4

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This is a sample blog post. Lorem ipsum I can’t remember the rest of lorem ipsum and don’t have an internet connection right now. Testing testing testing this blog post. Blog posts are cool.

Blog Post number 3

less than 1 minute read

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Blog Post number 2

less than 1 minute read

Published:

This is a sample blog post. Lorem ipsum I can’t remember the rest of lorem ipsum and don’t have an internet connection right now. Testing testing testing this blog post. Blog posts are cool.

Blog Post number 1

less than 1 minute read

Published:

This is a sample blog post. Lorem ipsum I can’t remember the rest of lorem ipsum and don’t have an internet connection right now. Testing testing testing this blog post. Blog posts are cool.

portfolio

projects

Real-Time Parameter Estimation and Prediction-Based Control for Aircraft Pitch Dynamics

Graduate Course Project, National Cheng Kung University, ME 8601 Adaptive Control (Instructor: Ming-Shaung Ju), 2021

This project utilizes the recursive integral-operator-based least-squares (RLS) algorithm to estimate the system parameters for a aircraft pitch dynamics (textbook example). The simulation results show that the proposed RLS estimator enable to estimate the system parameters. By introduced the predicted states as the feedback states, the control performance is further improved.

System Parameter Identification of Quadrotor

Graduate Course Project, National Cheng Kung University, ES 7140 Applied System Identification (Instructor: Jer‑Nan Juang), 2021

This project uses the first-order integral method the identify the system parameter for a nonlinear quadrotor model. The simulation result indicates that the presented method can well identify the moment of inertia provide that the thrust model of the propellers is known.

Inversion-Based Trajectory Control for 3-DoF Quadrotor

Graduate Course Project, National Cheng Kung University, ME 8602 Feedforward Control (Instructor: Szu-Chi Tien), 2021

This research report propose a feedback-feedforward control architecture for a 3-DoF nonlinear quadrotor model which the relative degree is not well-defined and the system subject to the parameter uncertainties. The simulation results reveals that the proposed controller is capable of tracking the desired trajectory in the presence of modeling uncertainties.

Inspection UAV System Development

Industry Collaboration Research Project, China Steel Corporation, Dept. of Green Energy & System Integration Research & Development, National Cheng Kung University, Dept. of Aeronautics and Astronautics, Intelligent Embedded Control Laboratory, 2023

This research considered an indoor UAV environmental inspection in heavy industry. The feedback position, velocity, and orientation rely on the vSLAM sensor to online estimate the pose of UAV in space. The following video demonstrates the quadrotor position control experiments using the vSLAM sensor.

publications

Super-Twisting Sliding Mode Control Law Design for Attitude Tracking Task of a Spacecraft via Reaction Wheels

Published in Mathematical Problems in Engineering, 2021

This paper applies the super-twisting sliding mode algorithm to design the control law for a spacecraft attitude control problem. The governing equations and the control allocation law of the pyramid type reaction wheel configuration are derived. The simulation results reveal that the superior tracking performance of the proposed controller in the presence of unknown external disturbances.

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Parameters identification of nonlinear Lorenz chaotic system for high-precision model reference synchronization

Published in Nonlinear Dynamics, 2021

This paper proposes a model reference adaptive control law to perform the synchronization control for the Lorenz chaotic system. Several system identification techniques are presented to identify the system parameters of the Lorenz system. With the aid of the identified parameters, the high-precision synchronization performance is achieved.

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Development of a Full Orientation Flight Robotics: Dynamics Modeling, Analysis, and Control Design

Published in IEEE Access, 2023

This study propose a novel flight robotics which is capable of achieving the arbitrary flight pose in six-degrees-of-freedom space. It uses multiple propellers to generate control force and torque. The corresponding control allocation algorithm is proposed in the sense of minimal energy consumption. The simulation results reveal the flight feasibility of the proposed novel flight robotics.

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talks

teaching

Teaching experience 1

Undergraduate course, University 1, Department, 2014

This is a description of a teaching experience. You can use markdown like any other post.

Teaching experience 2

Workshop, University 1, Department, 2015

This is a description of a teaching experience. You can use markdown like any other post.