A new type of rocket engine ground sensing and test system based on compressive sensing

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

This paper intends to solve the undersampling problem in the rocket engine experimental data sampling process. It starts with an overview of rocket engine experimental data sampling process fundamentals and the compressive sensing theory, including the sparse representation, the measurement matrix and the reconstruction algorithms. An abecedarian research centering on the pressure signal generated in the combustion chamber instable combustion model is used to explore basic procedures of processing both pure and noisy signal under the framework of compressive sensing, the analysis of the signal sparsity and the design of reconstruction algorithms. Numerical experiments verify the possibility and feasibility of compressive sensing in processing rocket engine experimental data. Finally, a new type of rocket engine ground sensing and test system and its hardware implementation are introduced.

Original languageEnglish
Title of host publication2015 IEEE International Conference on Mechatronics and Automation, ICMA 2015
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages132-138
Number of pages7
ISBN (Electronic)9781479970964
DOIs
StatePublished - 2 Sep 2015
Event12th IEEE International Conference on Mechatronics and Automation, ICMA 2015 - Beijing, China
Duration: 2 Aug 20155 Aug 2015

Publication series

Name2015 IEEE International Conference on Mechatronics and Automation, ICMA 2015

Conference

Conference12th IEEE International Conference on Mechatronics and Automation, ICMA 2015
Country/TerritoryChina
CityBeijing
Period2/08/155/08/15

Keywords

  • Compressive sensing
  • Hardware implementation
  • Numerical experiment
  • Rocket engine

Fingerprint

Dive into the research topics of 'A new type of rocket engine ground sensing and test system based on compressive sensing'. Together they form a unique fingerprint.

Cite this