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Title: Design and Testing of a Sensor Data Processing Unit for Dual-Control Missile Demonstrator
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The article discusses aspects of the design and testing of a sensor data processing unit whose function relates to the static and dynamic stabilization of a missile airframe. The authors present a mathematical model of dual-control missile dynamics, along with the autopilot implemented based on two feedback loops – from acceleration and from angular rate of the airframe. The draft of the sensor data processing unit is presented in the form of three PCB packages, with connections for the installation of electronic components. In addition, a laboratory stand used in the experimental research, as well as selected results for the device are described.
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Warszawa
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Identifier:
oai:ribes-88.man.poznan.pl:2553
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Keywords:
electronic circuit design, signal processing, autopilot, dual-control missile
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Last modified:
Sep 25, 2025
In our library since:
Sep 25, 2025
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0
All available object's versions:
https://ribes-88.man.poznan.pl/publication/2865
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| Edition name | Date |
|---|---|
| Design and Testing of a Sensor Data Processing Unit for Dual-Control Missile Demonstrator | Sep 25, 2025 |
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