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Mark B. Tischler
Mark B. Tischler
US Army
在 mail.mil 的电子邮件经过验证
标题
引用次数
引用次数
年份
Aircraft and rotorcraft system identification
MB Tischler, RK Remple
American Institute of Aeronautics and Astronautics, 2012
8862012
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
4032002
System identification of small-size unmanned helicopter dynamics
B Mettler, MB Tischler, T Kanade
Annual Forum Proceedings- American Helicopter Society 2, 1706-1717, 1999
3151999
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
2311992
Advances in aircraft flight control
MB Tischler
crc press, 1996
1601996
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
1222001
System identification methods for aircraft flight control development and validation
MB Tischler
Advances in aircraft flight control, 35-69, 2018
1172018
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
1022000
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
932017
Frequency-response identification of XV-15 tilt-rotor aircraft dynamics
MB Tischler
Stanford University, 1987
881987
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
861997
System identification requirements for high-bandwidth rotorcraft flight control system design
MB Tischler
Journal of Guidance, Control, and Dynamics 13 (5), 835-841, 1990
771990
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
732004
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
701999
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
681993
Digital control of highly augmented combat rotorcraft
MB Tischler
681987
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
672004
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
652017
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
551993
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
532005
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