Dissertation > Excellent graduate degree dissertation topics show

Design and Experimentation of Micro Impulse Jet Engine and Its Control Circuit

Author: ZhengYi
Tutor: TaoGang
School: Nanjing University of Technology and Engineering
Course: Weapons systems and the use of engineering
Keywords: micro impulse jet engine jet trajectory correction execute mechanism infantry rocket grenade AVR single chip
CLC: V433
Type: Master's thesis
Year: 2008
Downloads: 173
Quote: 1
Read: Download Dissertation

Abstract


Accurate strike has been a main character of modern warfare. Endue conventional ammunition with accurately strike ability is the trend of ammunition development, and trajectory correction is an effective means. In this dissertation, we focus the work on the execute mechanism of the trajectory correction rocket grenade, which is one of the key technology. A new type of trajectory correction execute mechanism - micro impulse jet engine - was put forward that is used in the infantry rocket grenade. A control circuit was designed for calculating and controlling the trajectory of the rocket grenade according to the working characteristics of the micro impulse jet engine and semi-active laser guider.The working principle of the correcting micro impulse jet engine was expatiated, and a prototype was worked out. The result of thrust test showed that the thrust value reached 1.425N while the compressed air pressure of engine was 0.65MPa. AVR single chip processor was applied in the control circuits which integrates the functions of target signal processing from the guider, 6 jet engines controlling, trajectory calculating and parameter outputting by serial port. Test showed that it could carry out the correcting control function according to the trajectory information from the guider head, and the trajectory correction execute mechanism is feasible for infantry rocket grenade.

Related Dissertations

  1. Attitude Control Law Design Based on Blended Lateral Jets and Aerodynamic Control,V249.1
  2. Influence of over Fired Air on Gas-Solid Flows in a W-Shaped Flame Boiler,TK229
  3. Fabrication of Membrane Electrode Assembly for PEMFC,TM911.4
  4. Microfluidics pulse drive - control microarray spotting system design and experimental study,TN402
  5. Simulation Research on Hydraulic System of Extra-High Pressure Water Jet Equipment,TH137
  6. Theoretical and Experimental Study on the Kinetic Model of CSM Demulsification & Devolatilization by the Water-Jet Method,TQ331.4
  7. Basic Study on Jet Characteristics of Supersonic Coherent Jet Oxygen Lance,TF341
  8. Research on Face Recognition Based on AdaBoost Algorithm,TP391.41
  9. Design and Improvement of the Jet-mixing Nozzle Used in Chlorosulfonated Polyethylene Emulsion Devolatilization,TQ330.4
  10. The Study of Marketing Strategy of First Mandarin Business Aviation Company,F562
  11. Preparation and Characterization of Aligned Ultrafine Fibers by Stable Jet Electrospinning,TQ340.64
  12. Study of Mechanical Vibration Aided Submersed Gas- Jetting Edm,TG661
  13. Continuous hot dip galvanized strip stable transmission , heat transfer and organizational change behavior,TK124
  14. Sterilization of atmospheric pressure plasma jet and its,O539
  15. Research on linear plasma jet,O53
  16. Polyester and viscose blended yarn MVS yarn spinning process and its impact on the performance and structure of,TS104
  17. Powerful jet vortex spinning influencing factors and related technology research,TS104
  18. PI control algorithm based on fuzzy inkjet printer ink system design studies,TS803.6
  19. Quasi-linear optimal control smoothing in a one-dimensional trajectory correction command shells on the Application of,TJ012
  20. Research on Attitude Determination and Magnetic Control for Small Satellites,V448.2
  21. The Dayoushan Tunnel Through Xining West Foundation Reinforcement Technology Research,U455.4

CLC: > Aviation, aerospace > Aerospace ( Astronauts ) > Propulsion system ( engine, propeller ) > Engine control systems and devices
© 2012 www.DissertationTopic.Net  Mobile