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Research on Integrated Navigation Technology and Semi-Physical Simulation of Hypersonic Vehicle
Author: HuangWei
Tutor: CuiNaiGang
School: Harbin Institute of Technology
Course: Aircraft design
Keywords: Hypersonic vehicle Master-slave redundancy Multi - sensor information fusion Semi-physical simulation
CLC: V249.328
Type: Master's thesis
Year: 2010
Downloads: 138
Quote: 1
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Abstract
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Hypersonic vehicle as the research object , fully autonomous hypersonic vehicle navigation system , high-reliability , high-precision application requirements , the main from redundant inertial navigation / satellite / starlight multi- sensor data fusion technology integrated navigation system designed theory and simulation studies and theoretical research as the basis to build a semi- physical simulation platform , to stage experimental verification . The main contents of the paper include: First, the the hypersonic vehicle integrated navigation technology involved in space coordinate system , the the hypersonic vehicle space equations of motion is derived , the design of a hypersonic aircraft trajectory generator , the inertial navigation system of mathematical model and error propagation equation . Second, the method and characteristics of strapdown inertial navigation system device redundancy more comprehensive research and analysis . Based on the inertial element parity principle , the design of the main program from redundant inertial navigation system , inertial navigation system fault diagnosis , and to ensure the reliability of the core navigation device parity processing, inertial navigation device measurement information . Then, the information fusion of multi-source navigation sensor integrated navigation method . Principle and error characteristics of the navigation system of satellite navigation and Star the designed inertial / satellite , inertial / Star integrated navigation Kalman filter based filtering error covariance matrix Trace law principle of distribution , completed the integrated navigation federal filter design . Finally , in the above - mentioned research results based on build semi-physical simulation platform integrated navigation system based on GPS receiver , inertial navigation devices , the actual physical device , and this semi- physical simulation platform of integrated navigation performance verification analysis .
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CLC: > Aviation, aerospace > Aviation > Aircraft instrumentation,avionics, flight control and navigation > Flight control system and navigation > Navigation > Navigation system > Integrated Navigation System
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