Design and implementation of an adaptive Kalman filtering for the launcher of multiple launch rocket system-Reference-Cited by-同舟云学术

Design and implementation of an adaptive Kalman filtering for the launcher of multiple launch rocket system

Published:2017-12-21 Issue:3 Volume:32 Page:447-463
ISSN:0890-6327
Container-title:International Journal of Adaptive Control and Signal Processing
language:en
Short-container-title:Int J Adapt Control Signal Process

Author:

Li Bo¹,Rui Xiaoting¹^ORCID,Yang Fufeng¹,Wang Guoping¹

Affiliation:

1. Institute of Launch Dynamics; Nanjing University of Science and Technology; Nanjing 210094 China

Funder

Doctoral Program of Higher Education of China

Research Innovation Project for College Graduates of Jiangsu Province

Publisher

Wiley

Subject

Electrical and Electronic Engineering,Signal Processing,Control and Systems Engineering

Reference31 articles.

1. Vibration control for launcher of multiple launch rocket system based on transfer matrix method of multibody system;Zhan;Chin J Theor Appl Mech,2010

2. Design of vibration control of launcher for multiple launch rocket system;Zhan;J Vib Eng,2011

3. Research on design and actualization of vibration controlled system of launch guider of MLRS;He;Fire Control Command Control,2013

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Improved Adaptive Kalman-Median Filter for Line-Scan X-ray Transmission Image;Sensors;2022-07-02

2. On modeling and dynamics of a multiple launch rocket system;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-03-10

3. Adaptive Kalman filtering for closed-loop systems based on the observation vector covariance;International Journal of Control;2021-01-11

4. An improved adaptive unscented Kalman filter for estimating the states of in‐wheel‐motored electric vehicle;International Journal of Adaptive Control and Signal Processing;2019-10-23