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Article
Capture condition for endo-atmospheric interceptors steered by ALCS and ARCS
This contribution deals with capture condition for interceptor missiles steered by aero-lift control system (ALCS) and attitude reaction-jet control system (ARCS). With the guidance law derived from bounded di...
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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...
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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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Chapter and Conference Paper
Safety Control of Quadrotor by Control Barrier Function Based-on Data-Driven Hamilton Dynamics Model
The accurate trajectory tracking and obstacle avoidance task of quadrotor is a difficult problem, because its dynamics is difficult to accurately establish, resulting in complex controller design. In order to ...
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Article
Open AccessSpacecraft Pose Estimation Based on Different Camera Models
Spacecraft pose estimation is an important technology to maintain or change the spacecraft orientation in space. For spacecraft pose estimation, when two spacecraft are relatively distant, the depth informatio...
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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...