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Stability and autopilot system for airplane RC model
Čamaj, Peter ; Republic), (SAAB Technologies Czech (referee) ; Šebesta, Jiří (advisor)
The master thesis deals with design and realization of stabilizing and autopilot system, which is used in radio controlled model planes. The thesis contains a proposal of hardware platform, which is able to control the plane model based on data measured from a sensor system. Moreover, this thesis describes a software implementation of individual modules, which is measured the onboard values. The basic principles of stabilization and autonomous flight control are also summarized. In conclusion, the system is subjected to flight tests.
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Wireless Telemetry System for RC Model
Čamaj, Peter ; Prokopec, Jan (referee) ; Šebesta, Jiří (advisor)
This project deals with design and realization of wireless telemetry system, which is special used in model of plane on remote control. It solves software and hardware realization of the telemetry system, which is able to wirelessly transmit the measured cockpit values, which are clearly displayed on LCD and also represented by sound.
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Wireless Telemetry System for RC Model
Čamaj, Peter ; Prokopec, Jan (referee) ; Šebesta, Jiří (advisor)
This project deals with design and realization of wireless telemetry system, which is special used in model of plane on remote control. It solves software and hardware realization of the telemetry system, which is able to wirelessly transmit the measured cockpit values, which are clearly displayed on LCD and also represented by sound.
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Stability and autopilot system for airplane RC model
Čamaj, Peter ; Republic), (SAAB Technologies Czech (referee) ; Šebesta, Jiří (advisor)
The master thesis deals with design and realization of stabilizing and autopilot system, which is used in radio controlled model planes. The thesis contains a proposal of hardware platform, which is able to control the plane model based on data measured from a sensor system. Moreover, this thesis describes a software implementation of individual modules, which is measured the onboard values. The basic principles of stabilization and autonomous flight control are also summarized. In conclusion, the system is subjected to flight tests.
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