JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD
AE605PC: FLIGHT DYNAMICS AND CONTROL LAB
B.Tech III Year II Semester (R16)
Overview
1. BASIC ANATOMY OF AN AIRCRAFT: The main aim of this experiment is to have a control over all the control surfaces of an aircraft.
2. HELICOPTER FLIGHT: The main aim of this experiment is to understand the mechanism involved in helicopter flight. The helicopter control mechanism is not exactly the same as that of an aircraft control mechanism, one need to study the controls mechanism of helicopter in order to obtain pitch, roll, and yaw maneuver.
3. FLIGHT SIMULATOR: The main aim of this experiment is to understand the mechanism involved in an aircraft and helicopter using flying software. Analysis of different mission segments of an aircraft and helicopter will be done.
4. ANALYSIS OF A STEADY LEVEL MANEUVERS AND INSTANTANEOUS MANEUVERS USING 2-D ACCELEROMETER: The main of this experiment is to analyze the data given by accelerometer for Pull-up, Pull- down maneuvers and Steady level turn.
5. FLIGHT MECHANISMS OF AN AIRCRAFT USING AURDINO: The main aim of this experiment is to analyze the actuation mechanisms of an aircraft and helicopter using Aurdnio with the help of mission planner software. R16 B.TECH AERONAUTICAL ENGG.