This memorandum is the first in a series giving an account of the design and structure of the on−board computer system for controlling a model helicopter. The aircraft itself is designed by a research group of the Institut für Mess− und Regeltechnik of ETH Zürich. The computer is to stabilize the helicopter and to execute commands for flight movements. It receives inputs from various sensors and drives the necessary servos. The computer is built around an ARM processor and an FPGA
In this work the development of a engine’s governor for a light single seat helicopter is presented....
We modelled an aircraft based on the Airbus A320 and constructed a synthesisable flight control syst...
We modelled an aircraft based on the Airbus A320 and constructed a synthesisable flight control syst...
This memorandum provides the defining document of the programming language Oberon−SA, a subset of Ob...
We describe a compiler, and in particular its generated code, translating from Oberon to binary code...
The aim of this research project is to develop an autopilot system that enables the helicopter model...
International Telemetering Conference Proceedings / October 30-November 02, 1995 / Riviera Hotel, La...
This thesis will present work done to develop the hardware of a flight control system (FCS) for an u...
In this paper we will introduce the existing model of a helicopter for teaching dynamic systems. Lat...
The detailed system design of a small experimental autonomous helicopter is described. The system re...
Helicopter missions place strong demands on the precise control characteristics of aircraft, particu...
This paper describles a dsign and development of a PC-based controller of a mini aerial helicopter f...
This paper presents the results, achieved at the Aerospace Engineering Department Laboratories of t...
Abstract: Building a scalable and highly integrated systems is an important re-search direction and ...
This paper presents the hardware design and integration process employed to develop an Unmanned Airc...
In this work the development of a engine’s governor for a light single seat helicopter is presented....
We modelled an aircraft based on the Airbus A320 and constructed a synthesisable flight control syst...
We modelled an aircraft based on the Airbus A320 and constructed a synthesisable flight control syst...
This memorandum provides the defining document of the programming language Oberon−SA, a subset of Ob...
We describe a compiler, and in particular its generated code, translating from Oberon to binary code...
The aim of this research project is to develop an autopilot system that enables the helicopter model...
International Telemetering Conference Proceedings / October 30-November 02, 1995 / Riviera Hotel, La...
This thesis will present work done to develop the hardware of a flight control system (FCS) for an u...
In this paper we will introduce the existing model of a helicopter for teaching dynamic systems. Lat...
The detailed system design of a small experimental autonomous helicopter is described. The system re...
Helicopter missions place strong demands on the precise control characteristics of aircraft, particu...
This paper describles a dsign and development of a PC-based controller of a mini aerial helicopter f...
This paper presents the results, achieved at the Aerospace Engineering Department Laboratories of t...
Abstract: Building a scalable and highly integrated systems is an important re-search direction and ...
This paper presents the hardware design and integration process employed to develop an Unmanned Airc...
In this work the development of a engine’s governor for a light single seat helicopter is presented....
We modelled an aircraft based on the Airbus A320 and constructed a synthesisable flight control syst...
We modelled an aircraft based on the Airbus A320 and constructed a synthesisable flight control syst...