| Title |
Trumpo nuotolio raketos valdymo sistemos kūrimas ir tyrimas / |
| Translation of Title |
Development and research of short range missile control system. |
| Authors |
Baranauskas, Gediminas |
| Full Text |
|
| Pages |
61 |
| Keywords [eng] |
short-range missile ; control system ; accelerometer ; gyroskope |
| Abstract [eng] |
The research and review was done about modern short-range missiles and determine the most important parameters influencing their management. After computer analysis of the air flow, the changes in the forces acting on the rocket was determines. During the analysis it was taken into account the different speeds, the wing geometry, angles of attack and the impeller position of influence missile operating force and torque of the center of gravity. According to this data was decided to develop rapidly responsive system that is managed by its wing-mounted front. Control system and calculation algorithm was developed. Great attention was paid to the sensor signal processing and aimed to create a more precise functional orientation system. In order to achieve a coherent and smoothly functioning dynamic parameters output by integration, the system was divided into 2 parts: the orientation and execution. Sensors and actuators for the system was selected. Research carried out to investigate the accelerometers and gyroscope. These studies established their errors and usage characteristics. |
| Dissertation Institution |
Kauno technologijos universitetas. |
| Type |
Master thesis |
| Language |
Lithuanian |
| Publication date |
2015 |
