Aircraft and rotorcraft system identification MB Tischler, RK Remple American Institute of Aeronautics and Astronautics, 2012 | 941 | 2012 |
System identification modeling of a small‐scale unmanned rotorcraft for flight control design B Mettler, MB Tischler, T Kanade Journal of the American helicopter society 47 (1), 50-63, 2002 | 395 | 2002 |
System identification of small-size unmanned helicopter dynamics B Mettler, MB Tischler, T Kanade Annual Forum Proceedings- American Helicopter Society 2, 1706-1717, 1999 | 311 | 1999 |
Frequency‐response method for rotorcraft system identification: flight applications to BO 105 coupled rotor/fuselage dynamics MB Tischler, MG Cauffman Journal of the American Helicopter Society 37 (3), 3-17, 1992 | 234 | 1992 |
Advances in aircraft flight control MB Tischler crc press, 1996 | 165 | 1996 |
The micro craft iSTAR micro air vehicle: Control system design and testing L Lipera, JD Colbourne, MB Tischler, MH Mansur, MC Rotkowitz, ... Annual Forum Proceedings-American Helicopter Society 57 (2), 1998-2008, 2001 | 124 | 2001 |
System identification methods for aircraft flight control development and validation MB Tischler Advances in aircraft flight control, 35-69, 2018 | 121 | 2018 |
Practical methods for aircraft and rotorcraft flight control design: an optimization-based approach MB Tischler, T Berger, CM Ivler, MH Mansur, KK Cheung, JY Soong American Institute of Aeronautics and Astronautics, Inc., 2017 | 112 | 2017 |
Attitude control optimization for a small-scale unmanned helicopter B Mettler, T Kanade, M Tischler, W Messner AIAA guidance, navigation, and control conference and exhibit, 4059, 2000 | 101 | 2000 |
Frequency-response identification of XV-15 tilt-rotor aircraft dynamics MB Tischler Stanford University, 1987 | 93 | 1987 |
Conduit-a new multidisciplinary integration environment for flight control development M Tischler, J Colbourne, M Morel, D Biezad, W Levine, V Moldoveanu, ... Guidance, navigation, and control conference, 3773, 1997 | 89 | 1997 |
System identification requirements for high-bandwidth rotorcraft flight control system design MB Tischler Journal of Guidance, Control, and Dynamics 13 (5), 835-841, 1990 | 79 | 1990 |
Rapid frequency-domain modeling methods for unmanned aerial vehicle flight control applications CR Theodore, MB Tischler, JD Colbourne Journal of Aircraft 41 (4), 735-743, 2004 | 78 | 2004 |
A multidisciplinary flight control development environment and its application to a helicopter MB Tischler, JD Colbourne, MR Morel, DJ Biezad IEEE Control Systems Magazine 19 (4), 22-33, 1999 | 73 | 1999 |
System identification and controller optimization of a quadrotor unmanned aerial vehicle in hover W Wei, MB Tischler, K Cohen Journal of the American Helicopter Society 62 (4), 1-9, 2017 | 70 | 2017 |
Digital control of highly augmented combat rotorcraft MB Tischler | 70 | 1987 |
High‐order state space simulation models of helicopter flight mechanics FD Kim, R Celi, MB Tischler Journal of the American Helicopter Society 38 (4), 16-27, 1993 | 69 | 1993 |
Empirically derived helicopter response model and control system requirements for flight in turbulence JA Lusardi, MB Tischler, CL Blanken, SJ Labows Journal of the American Helicopter Society 49 (3), 340-349, 2004 | 68 | 2004 |
Nonlinear inversion control for a ducted fan UAV C Spaulding, M Mansur, M Tischler, R Hess, J Franklin AIAA atmospheric flight mechanics conference and exhibit, 6231, 2005 | 56 | 2005 |
Forward flight trim and frequency response validation of a helicopter simulation model FD Kim, R Celi, MB Tischler Journal of Aircraft 30 (6), 854-863, 1993 | 56 | 1993 |