1 |
Edwards, C., Spurgeon, S. K. and Akoachere, A., "A Sliding Mode Static Output Feedback Controller Based on Linear Matrix Inequalities Applied to an Aaircraft", Journal of Dynamic Systems, Measurement, and Control, Vol. 122, 2000, pp. 656-662. DOI: 10.1115/1.1316786
DOI
|
2 |
Fletcher, L. R., "Output Feedback Matrices in the Presence of Direct Feedthrough", International Journal of Systems Science, Vol. 12, No. 12, 1981, pp. 1493-1495. DOI: 10.1080/00207728108963834
DOI
|
3 |
Fletcher, L. R., "On Pole Placement in Linear Multivariable Systems with Direct Feedthrough: I. Theoretical Considerations", International Journal of Control, Vol. 33, No. 4, 1981, pp. 739-749. DOI: 10.1080/00207178108922952
DOI
|
4 |
Fletcher, L. R., "On Pole Placement in Linear Multivariable Systems with Direct Feedthrough: II. Computational Considerations", International Journal of Control, Vol. 33, No. 6, 1981, pp. 1147-1154. DOI: 10.1080/00207178108922982
DOI
|
5 |
Skogestad, S. and Postlethwaite, I., Multivariable Feedback Control: Analysis and Design, 2nd ed., John Wiley & Sons Ltd, England, 2005. DOI: 10.1109/MCS.2007.284514
|
6 |
Pomfret, A., Ensor, J. and Clarke, T., "Eigenstructure Assignment for Semi-Proper Systems: Pseudo-State Feedback", Proceedings of the 16th IFAC World Congress, Prague, Czech, July 2005. DOI: 10.3182/20050703-6-CZ-1902.00627
DOI
|
7 |
Gustafson, J. A., "Control of a Large Flexible Space Structure Using Multiple Model Adaptive Algorithms", USA, 1991.
|
8 |
Fitch, J. A., "Multiple Model Adaptive Control of a Large Flexible Space Structure with Purposeful Dither for Enhanced Identifiability," USA, 1993.
|
9 |
Kokotovic, P. V., O'Malley Jr., R. E. and Sannuti, P., "Singular Perturbations and Order Reduction in Control Theory - an Overview", Automatica, Vol. 12, 1976, pp. 123-132. DOI:10.1016/0005-1098(76)90076-5
DOI
|
10 |
Stevens, B. L., Lewis, F. L. and Al-Sunni, F. "Aircraft Flight Controls Design Using Output Feedback", Journal of Guidance, Control and Dynamics, Vol. 15, No. 2, 1992, pp. 238-246. DOI: 10.2514/3.20824
DOI
|
11 |
Stevens, B. L. and Lewis, F. L., Aircraft Control and Simulation, John Wiley & Sons Inc, United States, 1992.
|
12 |
Tsai, J. S. H., Wang, C. T. and Shieh, L. S., "Model Conversion and Digital Redesign of Singular Systems", Journal of the Franklin Institute, Vol. 330, No. 6, 1993, pp. 1063-1086. DOI: 10.1016/0016-0032(93)90065-3
DOI
|
13 |
Wang, J. H., Tsai, J. S. H., Chen, Y. C., Guo, S. M. and Shieh, L. S., "An Active Low-Order Fault-Tolerant State Space Self-Tuner for the Unknown Sample-Data Linear Regular System with an Input-Output Direct Feedthrough Term", Applied Mathematical Sciences, Vol. 6, No. 97, 2012, pp. 4813-4855.
|
14 |
Kaynes, I. W. and Fry, D. E., "The Initial Design of Active Control Systems for a Flexible Aircraft", Proceeding of AGARD Conference, No. 354, 1983.
|
15 |
Ko, S. and Bitmead, R., "Optimal Control for Linear Systems with State Equality Constraints", Automatica, Vol. 43, No. 9, 2007, pp. 1573-1582. DOI: 10.1016/j.automatica.2007.01.024
DOI
|
16 |
Athans, M. and Schweppe, F. C., Gradient Matrices and Matrix Calculations, Technical Note 1965-53, Massachusetts Institute of Technology Lexington Lincoln Laboratory, November 1965.
|
17 |
Herrmann, G., Spurgeon, S. K. and Edwards, C., "A Robust Sliding-Mode Output Tracking Control for a Class of Relative Degree Zero and Non-Minimum Phase Plants: a Chemical Process Application", International Journal of Control, Vol. 74, No. 12, 2001, pp. 1194-1209. DOI: 10.1080/00207170110061040
DOI
|