[1] Kokotovic, P., Khalil, H., O’Reilly, J., “Singular Perturbation
Methods in Control”, Academic press, London, 1986.
[2] Innocenti, M., Greco, L., Pollini, L., “Sliding Mode Control for Two-Time Scale Systems: Stability Issues”, Automatica (39), pp. 273-280,
2003.
[3] Oloomi, H., Shafai, B., “Realization Theory for Two-Time Scale
Distributions through Approximation of Markov Parameters”,
International Journal of Systems Science, vol. 39, No. 2, pp. 127-138,
February 2008.
[4] Babister, A.W., “Aircraft Dynamic Stability and Response”,
Pergamon, 1980.
[5] Gajic, Z., Lim, M., “Optimal Control of Singular Perturbed Linear
Systems and Application”, Marcel Decker, New York 2001.
[6] Menon, P. K., Ohlmeyer, E. J., “Integrated Design of Agile Missile
Guidance And Autopilot Systems”, Presented at the 1999
Mediterranean Control Conference, June 28-30, Haifa, Israel.
[7] Blakelock, J.H., “Automatic Control of Aircraft and Missiles”, John
Wiley & Sons Inc., 1965.
[8] Ohlmeyer, E. J., “Root-Mean-Square Miss Distance of Proportional
Navigation Missile Against Sinusoidal Target”, Journal of Guidance,
Control and Dynamics, Vol. 19, pp.563-568, May-June 1996.
[9] Calise A.J., “Singular Perturbation methods for Variational Problems
in Aircraft Flight”, IEEE Transaction, Automatic Control, Vol. 1, AC-21, 1976.
[10] Subbaram Naidu, D., Calise, A.J., “Singular Perturbations and Time
Scales in Guidance and Control of Aerospace Systems: a Survey”,
Journal of Guidance, Control and Dynamics, vol. 24, No. 6, pp. 1057-1070, 2001.
[11] Faruqi, F.A., “State Space Model for Autopilot Design of Aerospace
Vehicles”, Weapons System Division, Defense Science and
Technology Organizations, Unclassified at 2007, DSTO-TR-1990
[12] HU Yenan, SUN Fuchun, LIU Huaping, WU Hao, “ε-Dependent
Controllability for Two-Time-Scale Systems”, Tsinghua Science and
Technology, Vol. 14, Num. 2, pp.271-280, April 2009.
[13] Maciejowski, J.M., “Multivariable Feedback Design”, Addison-Wesley Publication Co., 1989.
[14] Tavasoli, A., Eghtesad, M., Jafarian, H., “Two-Time Scale Control
and Observer Design for Trajectory Tracking of Two Cooperating
Robot manipulators Moving a Flexible Beam”, Journal of Robotics
and Autonomous Systems (57), pp. 212-221, 2009.
[15] Van Willigenburg, L.G., De Koning, W.L., Optimal Reduced-Order
Compensators for Time-Varying Discrete-Time Systems with
Deterministic and White Parameters, Automatica, vol. 35, pp. 129–
138, 1999.
[16] Bernstein, D.S., Davis, L.D., Hyland, D.C., The Optimal Projection
Equations for Reduced-Order Discrete-Time Modeling Estimation and
Control, Journal of Guidance Control and Dynamics, vol. 9 (3), pp.
288–293, 1986.
[17] Kwakernaak, H., Sivan, R., Linear Optimal Control Systems, First
Edition. Wiley-Interscience, 1972.
[18] Svendenius, J., Wittenmark, B., Review of Wheel Modeling and
Friction Estimation, Department of Automatic Control, Lund Institute
of Technology, 2003.
[19] Ozkan, B., Dynamic Modeling, Guidance and Control of Homing
Missiles, A Thesis Submitted to the Graduate School of Natural and
Applied Sciences, Middle East Technical University, 2005.
[20] Military Handbook, Missile Flight Simulation, Department of
Defense, United States of America, MIL-HDBK-1211(MI), Metric
Version, Classification: APR.
[21] Siouris, G.M., Missile Guidance and Control Systems, Avionics and
Weapon Systems, Wright-Patterson AFB, USA, 2004.
[22] Westrum, R., Sidewinder-Creative missile development at China
Lake, Naval Ins. Press, 1999.
[23] Yanushevsky, R., Modern Missile Guidance, CRC Press, 2007.
[24] Zarchan, P., Tactical and Strategic Missile Guidance, 5
th
Edition,
Progress in Astronautics and Aeronautics, American Institute of
Aeronautics and Astronautics (AIAA), 2007.
[25] Shneydor, N.A., Missile Guidance and Pursuit: Kinematics, Dynamics
and Control, Horwood Publication, 1998.
Thank you for copying data from http://www.arastirmax.com