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Chapter
Simple Electroaerodynamic Aircraft Testing with Multistage Staggered Arrangement of the Electrodes
Electroaerodynamic (EAD) devices use corona-induced ionic winds for in-atmosphere propulsion, from which EAD aircraft are derived with the advantages of low mechanical fatigue, low noise and zero carbon emissi...
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Chapter
Rapid Trajectory Optimization of Continuous-Low-Thrust Spacecraft Based on Bezier Shape Function and Inverse Dynamics
Deep space exploration missions are a great fit for continuous-thrust spacecraft because of their benefits of high specific impulse and extended operating period. However, when it comes to tackling the traject...
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Chapter and Conference Paper
Linear Gaussian Processes for Data-Efficient Robot Dynamics Learning
This paper proposes a linear Gaussian Process learning framework which can be used in the both of semi-parametric and non-parametric models. Inspired by the linear relationship in Euler–Lagrange equation, this...
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Chapter and Conference Paper
Pose Estimation Algorithm for Helicopter Landing Based on YOLO and PNP
Pose estimation measured by the camera is increasingly used in helicopter landing. We present a pose estimation algorithm for autonomous landing. You Only Look Once (YOLO) algorithm is extended to estimate the...
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Article
Coupled attitude-vibration analysis of an E-sail using absolute nodal coordinate formulation
In this study, the effects of solar wind on an electric sail (E-sail) are modeled and analyzed using an absolute nodal coordinate formulation (ANCF). First, the thrust of the charged metal tether that makes up...