Abstract

This paper has proposed effective measuring methods for feature points aiming at the unique and particular structure of “non-holosymmetric” carrier rocket, using the rocket imaging information obtained through optical measurement in launch vehicle range, and established a mathematic model about the threaten influence of the carrier rocket on the tower at taking-off stage, and conducted qualitative and quantitative analysis; At the same time, the calculation model of rocket’s posture speed and acceleration established is used for analyzing the carrier rocket’s flying state. Availability of the method has been proved through actual application, which has provided effective technical support for performance analysis of the carrier rocket’s vertical flight stage.

Details

Title
Performance Evaluation for Optical Measurement-Based Non-Holosymmetric Rocket at Taking-Off Stage
Author
Cui, Shuhua 1 ; Shen, Si 2 ; Lin, Haichen 2 ; Kang, Yuanyuan 1 ; Qing, Bo 2 

1  State Key Laboratory of Astronautic Dynamics, Xi’an 710043, China 
2  Xi’an Satellite Control Center, Xi’an 710043 China 
Publication year
2018
Publication date
Dec 2018
Publisher
IOP Publishing
ISSN
17578981
e-ISSN
1757899X
Source type
Scholarly Journal
Language of publication
English
DOI
https://doi.org/10.1088/1757-899X/466/1/012057
ProQuest document ID
2557240840
Copyright
© 2018. This work is published under http://creativecommons.org/licenses/by/3.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.