A reliable data-driven model for Ablative Pulsed Plasma Thruster-Reference-Cited by-同舟云学术

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A reliable data-driven model for Ablative Pulsed Plasma Thruster

Published:2020-10 Issue: Volume:105 Page:105953
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Hossain Noman,Wang Ningfei,Sun Guorui,Li Hang,Wu Zhiwen

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference26 articles.

1. Pulsed plasma thruster;Burton,1998

2. UAV aerodynamic design involving genetic algorithm and artificial neural network for wing preliminary computation;Rebhi,2019

3. Neural network-based adaptive sliding mode control design for position and attitude control of a quadrotor UAV;Razmi;Aerosp. Sci. Technol.,2019

4. Morphing control of a new bionic morphing UAV with deep reinforcement learning;Xu;Aerosp. Sci. Technol.,2019

5. Repetitively enhanced neural networks method for complex engineering design optimisation problems;Van Nguyen;Aeronaut. J.,2015

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1. Applications of deep learning to selected aerospace systems;Aerospace Systems;2024-04-08

2. A comparative study on the different energy supply modes for a micro-cathodic arc thruster;Journal of Applied Physics;2023-07-18

3. Burning characteristics and combustion wave model of AP/AN-based laser-controlled solid propellant;Energy;2022-08

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