Introduction to Avionics Systems
Springer Science & Business Media, 23 Ιουν 2011 - 530 σελίδες
Introduction to Avionic Systems, Third Edition explains the basic principles and underlying theory of the core avionic systems in modern civil and military aircraft, comprising the pilot’s head-up and head-down displays, data entry and control systems, fly by wire flight control systems, inertial sensor and air data systems, navigation systems, autopilots and flight management systems. The implementation and integration of these systems with current (2010) technology is explained together with the methods adopted to meet the very high safety and integrity requirements. The systems are analysed from the physical laws governing their behaviour, so that the system design and response can be understood and the performance examined. Worked examples are given to show how the theory can be applied and an engineering “feel” gained from a simplified model. Physical explanations are also set out and the text is structured so that readers can “fast forward” through the maths, if they so wish. Introduction to Avionic Systems, Third Edition meets the needs of graduates, or equivalent, entering the aerospace industries who have been educated in a wide range of disciplines, for example, electronic engineering, computing science, mathematics, physics, mechanical and aeronautical engineering. It also meets the needs of engineers at all levels working in particular areas of avionics who require an understanding of other avionic systems. Technology is continually advancing and this new third edition has been revised and updated and the presentation improved, where appropriate, The systems coverage has also been increased and a new section on helicopter flight control added.
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Chapter 2 Displays and ManMachine Interaction
Chapter 3 Aerodynamics and Aircraft Control
Chapter 4 FlybyWire Flight Control
Chapter 5 Inertial Sensors and Attitude Derivation
Chapter 6 Navigation Systems
Chapter 7 Air Data and Air Data Systems
Chapter 8 Autopilots and Flight Management Systems
Άλλες εκδόσεις - Προβολή όλων
accelerometer accuracy achieved actuator aerodynamic air data aircraft airspeed altitude angle of incidence angular automatic autopilot avionic systems axes axis BAE Systems bank angle basic calibrated airspeed Chapter closed-loop cockpit collimating configuration control surface damping data bus deflection derivative due display dynamic Earth’s effect enables equation error Euler Euler angles Eurofighter Typhoon failure FBW system fibre flight control system flight management system flight path force frequency GPS satellite heading height helicopter helmet hence inertial input integrity Kalman filter laser lift force loop Mach number magnetic manoeuvre measured mode monitoring motion navigation systems operation optical output phase pilot pitch rate position radar reference response resulting roll rate rotation rotor Schuler tuning shown in Figure signal speed stability augmentation static pressure strap-down sub-systems tailplane temperature transfer function true airspeed typical vector vertical wing