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This presentation by Christian Müller delves into altitude control systems for flight applications. It covers motivation behind the technology, essential basics of micro-copters, and the crucial role of various sensors, including GPS, ultrasonic, and pressure sensors. The hardware structure is outlined using ATmega644P, while system simulations and controller types (P, I, D) are discussed. The use of ultrasonic sensors for material detection and echos are highlighted. The conclusion emphasizes the significance of simulation and systematic design for effective altitude control and safety measures.
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Altitude control for a flight system Christian Müller 05.11.2012
Agenda • Motivation • Basics • Sensors • Hardware-structure • Altitude control • Models and simulation • Ultrasonic sensor • Conclusion
Motivation • Wide range of applications • Observation, inspections, measurements • Cost and resource savings • Protection of human life
Basics • Micro-copter • Functions: • Take off / land • Hover • Control position and height • Collision avoidance • Payload
Sensorsystems • GPS and compass • LEA-6S (ublox), CMPS03 (Devantech) • Acceleration and gyroscopes • LIS344ALH (STMicroelectronics), Murata ENC-03 • Air pressure • MPX 4115A (Freescale)
Hardware-structure • ATmega644P • Sirf Atlas V • Operating systems
Altitude control Formulas Model (MLDesigner) Simulation Code MC (Atmega)
Controller • Typesofcontrollers: • Proportional • Integral • Derivative Controller System
Ultrasonic sensor • SRF 05 • Specific problems: • Detection of different materials (fleece)
Ultrasonic sensor • Reflexions
Ultrasonic sensor • Echos from distant objects OUT IN
Conclusion • Simulation • Control unit design • Hardware • Implementation / test • Equal steps for other control systems (position, …)