Dissertation > Excellent graduate degree dissertation topics show

Study of Iterative Guidance for Long-Range Ballistic Missile

Author: WangDongLi
Tutor: CuiNaiGang
School: Harbin Institute of Technology
Course: Aircraft design
Keywords: Iterative guidance Optimal Control Accuracy analysis Need for speed
CLC: TJ761.3
Type: Master's thesis
Year: 2007
Downloads: 507
Quote: 0
Read: Download Dissertation

Abstract


In order to improve the guidance accuracy of long-range ballistic missiles and mobile launch capability , the iterative guidance method is applied to long-range ballistic missile guidance system , mainly to complete the following aspects of research . First ballistic missile guidance theory . Consider the long-range ballistic missiles of the Earth flat rate dynamics and kinematics equations . According to the characteristics of the missile in the actual flight dynamics and kinematics equations simplify . Use of the iterative guidance principle , determine the real-time solutions of the equations of motion . Optimal control using optimal control theory , while the introduction of the average gravitational simplified assumptions, the establishment of a long-range ballistic missile functionals . Analysis in a different terminal conditions , the feasibility of the iterative guided method , derived the optimal control of ballistic missile solution . Derive the to meet the missile shutdown conditions guided equations . Landing Error compensation in the case of considering the Earth flat rate Reentry air resistance on the virtual target . To determine the need for speed, and in accordance with the virtual target to determine the shutdown control function . Design simulation process , using MATLAB software development simulation program , long-range ballistic the iterative guidance mathematical simulation . Draw the corresponding simulation data , curve , and gives the analysis of the results . Finally , on the basis of the guidance simulation , using the Monte-Carlo statistical test method of the iterative guided guided precision made ??further statistical analysis . This paper made ??some studies to solve the problem of long-range ballistic missile mobile launchers Guidance and improve the accuracy of long-range ballistic missile hit , and guided Hit the accuracy of the statistical analysis , the study has some theoretical significance and practical value .

Related Dissertations

  1. Research on the Optimization of Laser Triangulation Device,TH744.5
  2. Optimal Synchronization Control of a Class of Underactuated Lagrangian Systems,TP13
  3. Design and Implementation of Rotational Inverted Pendulum Control System Based on Sliding Mode Observer,TP13
  4. Study on Hybrid Remanufacturing/Manufacturing Inventory Control System Based on PULL Strategy,F224
  5. Control of a Switched Reluctance Generator for Small Wind Power Systems,TM352
  6. Substation Voltage and Reactive Power Optimization Control Strategy and Implementation,TM761.1
  7. Luan River pulverized coal-fired power plant ash removal system design and system optimization selection,X773
  8. Wind power and pumped storage interconnected system stability and control,TV743
  9. Based on fuzzy reasoning annular multi -stage inverted pendulum modeling and control,TP13
  10. TRNSYS of a class -based Fuzzy Control Simulation of VAV system,TU831.3
  11. Aerospace dynamics of pseudo-spectral iterative solution,V412.41
  12. Research on Traffic Assignment Problems Based on Intelligent Optimization,O224
  13. Attitude Control Technology of a Small Video Satellite,V448.2
  14. Study on Application of Total Station in Highway Tunnel Deformation Measurement,U456.3
  15. Strength Reduction Finite Element Analysis of Soil Slope Stability,TU43
  16. The Study of Stochastic-parallel-gradient-descent Adaptive Optics Control Platform Based on DSP,O437
  17. Study on Optimal Control for Chaotic System Based on T-S Fuzzy Model,O232
  18. Optimal Control for Stable Solution of Repairable Human-Machine Systems,O232
  19. The Existence and Uniqueness of Classical Solutions and the Optimal Control Analysis for a Class of Nonlinear Mixed Forest Evolution Systems,O232
  20. Behavior Analysis and Optimal Control of Biological Population Dynamical Systems with Size-Structure,O232
  21. 400KA Aluminum Reduction Cell Energy Optimization Control System and Realization,TF821

CLC: > Industrial Technology > Arms industry > Rockets, missiles > Missile > Missiles : the range,the role of structural distinctions > Ballistic missile
© 2012 www.DissertationTopic.Net  Mobile