1. 1) Tischler, M. B. and Gauffman, M. G.: Frequency-Response Method for Rotorcraft System Identification: Flight Application to BO 105 Coupled Rotor/Fuselage Dynamics, J. Am. Helicopter Soc., 37, 3 (1992), pp. 3-17.
2. 2) Fu, K. H. and Kaletka, J.: Frequency-Domain Identification of BO105 Derivative Model with Rotor Degree of Freedom, 16th European Rotorcraft Forum, UK, 1990.
3. 3) La Civita, M., Papageorgiou, G., Messner, W. C. and Kanade, T.: Design and Flight Testing of a High-bandwidth H∞ Loop Shaping Controller for a Robotic Helicopter, Proceedings of the AIAA Guidance, Navigation, and Control Conference, Monterey, AIAA Paper 2002-4836, 2002.
4. 4) McFarlane, D. C. and Glover, K.: A Loop Shaping Design Procedure Using Synthesis, IEEE Trans. Autom. Control, 37, 6 (1992), pp. 759-769.
5. 5) ADS-33E-PRF, Aeronautical Design Standard Performance Specification Handling Qualities Requirements for Military Rotorcraft, United States Army Aviation and Missile Command, 2000.