On this page you will find supplementary materials to the book "Flugregelung" (Flight Control):

1. Matlab® scripts for example calculations,
2. An overview list with terms and definitions.

The scripts are based on Matlab® 2010b code. With this, the following can be calculated for the data of six example aircrafts provided in the appendix. These are:

• Derivatives
• State space representation
• Eigenvalues
• Frequency Responses
• Root locus curves and
• Time responses

The source code is commented. To use the code with other Matlab® versions or in other computer algebra systems, such as Octave or SciLab, adaptations may be necessary.

The source code is intended exclusively for non-commercial use. Any industrial or commercial use of the source code requires the permission of the authors.

The files are continuously updated. So far available are:

1. Terms and Definitions (as of 01.12.2011)
2. Replacement sizes for longitudinal and lateral motion for the example aircrafts specified in Annex A2 (status: 30.10.2011)
3. Bode diagrams, step responses, pole/zero and root locus curves for the example aircrafts given in Annex A2 (as at 30.10.2011)
4. Erratum list (as of 30.10.2011)
5. Documentation on the calculation program "FR_calc" (as at 30.10.2011)
6. Calculation program "FR_calc" for the calculation of equivalent quantities, state space representation, eigenvalues, frequency responses, root locus curves and time responses (as of 30.10.2011)