Experimental research on initial disturbances of rocket

Zhen Chen*, Shi Hua Bi, Guang Pu Liu, Hong Xia Pan

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

1 Citation (Scopus)

Abstract

A laser measuring system for initial disturbances of rockets was developed based on "optical lever" principle. The composition and basic principle of the system are introduced briefly. In the system, the wavelength of semiconductor lasing light emitter is 650 nm, the resolution of the position sensitive detector (PSD) is 10-6 m and the measuring error is less than 2×10-5rad. A measuring experiment was carried out with 54 mm rocket using this system. The comparison with the simulation results show that the experimental results are rational and credible. Finally, an error analysis was made for the system.

Original languageEnglish
Pages (from-to)112-114
Number of pages3
JournalGuti Huojian Jishu/Journal of Solid Rocket Technology
Volume33
Issue number1
Publication statusPublished - Feb 2010

Keywords

  • Initial disturbances
  • Laser measuring system
  • Launcher of rocket
  • Optical lever

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