Flight Management System 1

Lecturer:

Tutor:

Supervisor:

Department of Control Engineering

Synopsis:

The overview and classification according to various criteria of flight management system is presented. Next theme is devoted to the aircraft dynamics derivation and their linearisation, followed by outer and states spaced description of longitudinal and lateral-directional aircraft motion. Then follow automatic flight systems-autopilot, their structure and design, for longitudinal and lateral-directional aircraft motion separately.

Requirements:

Syllabus of lectures:

1. Pilot's activity on the board during flight control. Flight management systems, their structure and classification

2. Aircraft dynamics, motion arround its centre of gravity, equations, their derivation, linearization

3. Longitudinal motion, complete and its approximations

4. Lateral/directional motion, complete and its approximations

5. State space analysis

6. Identification of aircraft dynamics from flight measurements

7. Computer support of aircraft dynamics analysis

8. Automatic control of aircraft dynamics - autopilots, their structure and classification

9. Flying-qualities specification, design requirements, methods of synthesis

10. Servomachanismus of autopilots, types P, I, PI

11. Design of damping ratio and natural frequency for the short-period mode

12. Automatic control of longitudinal aircraft motion

13. Lateral - directional aircraft motion uncoordinated and coordinated

14. Automatic control of lateral - directional aircraft motion

Syllabus of tutorials:

1. Status of laboratory, software enviroment

2. The first task: Servomechanismus with loaded shaft

3. Structral block scheme in Simulink

4. Computation of motor power via simulation

5. Discussion of result

6. The second task: Simulation of longitudinal motion

7. Analysis of aircraft dynamics and their presentation

8. The third task: Simulation of lateral/directional motion

9. Analysis of aircraft dynamics and their presentation

10. The fourth task: Design of autopilot in longitudinal control

11. Design of the damper for short-period mode

12. Design of stabilisator of angle of atack

13. Design of pitch angle stabilisation

14. Discussion of results

Study Objective:

Study materials:

[1] Blackelok, J., N.: Automatic Control of Aircraft and Missiles

[2] Roskam, J.: Airplane flight dynamics and automatic flight controls. Roskam Aviation and Eng. Corp., Kansas

Note:

Further information:

No time-table has been prepared for this course

The course is a part of the following study plans:

• Aerial Information and Control Systems - Magister Studies (compulsory course)
• Aerial Information and Control Systems - Magister Studies (compulsory course)