A closed-form solution for the design of lead-lag compensators based on an exact model-matching criterion is developed. Using the developed design tool, students are able to obtain lead-lag compensators in a fraction of the time that is required by traditional design methods.
TaylorJ. H.StrobelK. L., ‘Nonlinear control system design based on quasilinear system models,’ in Proceedings of American Control Conference, Boston, MA, 1985, pp. 1242–1247.
2.
OgataK., Modern Control Engineering, 2nd edn (Prentice Hall, Englewood Cliffs, NJ, 1990) p. 583.
3.
RowlandJ. R., Linear control systems (John Wiley, New York1986).
4.
JamesJ. R., ‘Considerations concerning the construction of an expert system for control system design,’ PhD dissertation, Renselaer Polytechnique Institute, 1986.
5.
TeixeiraM. C. M., ‘Direct expressions for Ogata's lead-lag design method using root locus,’IEEE Trans. Educ.37 (1994), 63–64.
6.
YeungK. S.WongK. W.ChenK. L., ‘A non-trial-and-error method for lag–lead compensator design,’IEEE Trans. Educ., 41 (1998), 76–80.
7.
YeungK. S.LeeK. H., ‘Universal design chart for linear time-invariant continuous-time and discrete-time compensators,’IEEE Trans. Educ., 43 (2000), 309–315.
8.
MarroG.ZanasiR., ‘New formulae and graphics for compensator design,’ in Proc. IEEE International Conference on Control Applications, Trieste, Italy, 1 (1998), 129–133.
9.
WangF.-Y.HuangY. H., ‘A non-trial-and-error method for phase-lead and phase-lag compensator design,’ in Proc. IEEE International Conference on Systems, Man and Cybernetics, Tucson, AZ, 3 (2001), 1654–1660.
10.
ChenC. F.ShiehL. S., ‘An algebraic method for control systems design,’Int. J. Control, 11 (1970), 717–739.
11.
PujaraL. R., ‘Computer-aided control systems design technique with applications to aircraft flying qualities,’AIAA J. Guidance, Control, Dynam., 11 (1988), 250–255.
12.
NassirharandA., ‘Factorization approach to control system synthesis,’AIAA J. Guidance, Control, Dynam.16 (1992), 402–105.
