Helicopter Dynamics and Flight Control
This module handbook serves to describe contents, learning outcome, methods and examination type as well as linking to current dates for courses and module examination in the respective sections.
Module version of SS 2013
There are historic module descriptions of this module. A module description is valid until replaced by a newer one.
|available module versions|
|WS 2013/4||SS 2013|
MW1402 is a semester module in German language at Master’s level which is offered in winter semester.
This Module is included in the following catalogues within the study programs in physics.
- Catalogue of non-physics elective courses
|Total workload||Contact hours||Credits (ECTS)|
|90 h||30 h||3 CP|
Content, Learning Outcome and Preconditions
Development of a dynamic helicopter model as a prerequisite for flying qualities analysis and
flight control system design
- Introduction: Basic differences between fixed wing and rotary wing aircraft
- Rotor aerodynamics in hover, vertical climb, and decent
- Rotor dynamics: Blade flapping and lagging
- Rotor forces in forward flight
- Trim conditions
- Equations of motion
- Eigenmodes and stability
- Dynamic coupling between airframe and rotor
Part 2: Helicopter Flight Control
Flight control system design based upon the helicopter model and flying qualities
- Functional requirements
- Control laws for command and stability augmentation
- Operational requirements
- Configuration of flight control system
moments are generated, by which the helicopter flying qualities are determined, i. e. stability,
controllability, and response to disturbances. The knowledge of the plant and the understanding
of how the plant is functioning are prerequisites for designing a control system with the
capability to improve the flying qualities. The knowledge on helicopter dynamics and flight
control gained by the lecture will serve as a basis for further studies on helicopter technology.
Courses, Learning and Teaching Methods and Literature
Courses and Schedule
|VO||2||Helicopter Dynamics and Flight Control”||
Responsible/Coordination: Abdelmoula, A.
Wed, 14:00–15:30, MW 2701m
Learning and Teaching Methods
Description of exams and course work
There is a possibility to take the exam in the following semester.