-
1
-
-
0000504387
-
Identification and hysteretic control influence operators representing smart actuators. I: Formulation
-
Banks, H. T., Kurdila, A. J., and Webb, G. (1997a). "Identification and hysteretic control influence operators representing smart actuators. I: Formulation." Math. Prob. Eng., 3, 287-328.
-
(1997)
Math. Prob. Eng.
, vol.3
, pp. 287-328
-
-
Banks, H.T.1
Kurdila, A.J.2
Webb, G.3
-
2
-
-
0031153647
-
Identification and hysteretic control influence operators representing smart actuators. II: Convergent approximations
-
Banks, H. T., Kurdila, A. J., and Webb, G. (1997b). "Identification and hysteretic control influence operators representing smart actuators. II: Convergent approximations." J. Intell. Mater. Syst. Struct., 8, 536-550.
-
(1997)
J. Intell. Mater. Syst. Struct.
, vol.8
, pp. 536-550
-
-
Banks, H.T.1
Kurdila, A.J.2
Webb, G.3
-
3
-
-
0030085534
-
Advances in the development of an intelligent helicopter rotor employing smart trailing-edge flaps
-
Ben-Zeev, O., and Chopra, I. (1996). "Advances in the development of an intelligent helicopter rotor employing smart trailing-edge flaps." Smart Mater. Struct., 5(1).
-
(1996)
Smart Mater. Struct.
, vol.5
, Issue.1
-
-
Ben-Zeev, O.1
Chopra, I.2
-
6
-
-
0017555588
-
Recent developments in rotary-wing aeroelasticity
-
Friedmann, P. (1977). "Recent developments in rotary-wing aeroelasticity." J. Aircr., 11, 1027-1041.
-
(1977)
J. Aircr.
, vol.11
, pp. 1027-1041
-
-
Friedmann, P.1
-
7
-
-
3042678031
-
Rotary wing aeroelastic scaling and its application to adaptive materials based actuation
-
American Institute of Aeronautics and Astronautics, Washington, D.C.
-
Friedmann, P. (1998). "Rotary wing aeroelastic scaling and its application to adaptive materials based actuation." Proc., 39th Structures, Structural Dynamics, and Materials Conference, Adaptive Structures Forum, American Institute of Aeronautics and Astronautics, Washington, D.C.
-
(1998)
Proc., 39th Structures, Structural Dynamics, and Materials Conference, Adaptive Structures Forum
-
-
Friedmann, P.1
-
8
-
-
0020649648
-
Formulation and solution of rotary-wing aeroelastic stability and response problems
-
Friedmann, P. P. (1983). "Formulation and solution of rotary-wing aeroelastic stability and response problems." Vertica, 7(2), 101-141.
-
(1983)
Vertica
, vol.7
, Issue.2
, pp. 101-141
-
-
Friedmann, P.P.1
-
9
-
-
0030682254
-
Hover testing of a small-scale rotor with on-blade elevons
-
American Helicopter Society, Alexandria, Va.
-
Fulton, M. V., and Ormiston, R. A. (1997). "Hover testing of a small-scale rotor with on-blade elevons." Proc., 53rd Annual Forum of the American Helicopter Society, American Helicopter Society, Alexandria, Va.
-
(1997)
Proc., 53rd Annual Forum of the American Helicopter Society
-
-
Fulton, M.V.1
Ormiston, R.A.2
-
10
-
-
0031651091
-
Small scale rotor experiments with on-blade elevons to reduce blade vibratory loads in forward flight
-
American Helicopter Society, Alexandria, Va.
-
Fulton, M. V., and Ormiston, R. A. (1998). "Small scale rotor experiments with on-blade elevons to reduce blade vibratory loads in forward flight." Proc., 54th Annual Forum of the American Helicopter Society, American Helicopter Society, Alexandria, Va.
-
(1998)
Proc., 54th Annual Forum of the American Helicopter Society
-
-
Fulton, M.V.1
Ormiston, R.A.2
-
11
-
-
0032623991
-
Preliminary testing of a mach scaled active rotor blade with a trailing edge servo-flap
-
International Society for Optical Engineering, Bellingham, Wash
-
Hall, S. R., and Prechtl, E. F. (1998). "Preliminary testing of a mach scaled active rotor blade with a trailing edge servo-flap." SPIE Paper No. 3668-03, International Society for Optical Engineering, Bellingham, Wash.
-
(1998)
SPIE Paper No. 3668-03
, vol.3668
, Issue.3
-
-
Hall, S.R.1
Prechtl, E.F.2
-
13
-
-
13944276967
-
Chapter 9: Relaxed controls and a class of active material actuator materials
-
G. Tao, ed., Springer, London
-
Kurdila, A. J. (2001). "Chapter 9: Relaxed controls and a class of active material actuator materials." Adaptive control of nonsmooth dynamic systems, G. Tao, ed., Springer, London, 249-271.
-
(2001)
Adaptive Control of Nonsmooth Dynamic Systems
, pp. 249-271
-
-
Kurdila, A.J.1
-
14
-
-
0031274473
-
Compensation for distributed hysteresis operators in active structural systems
-
Kurdila, A. J., and Webb, G. (1997). "Compensation for distributed hysteresis operators in active structural systems." J. Guid. Control Dyn., 20(6).
-
(1997)
J. Guid. Control Dyn.
, vol.20
, Issue.6
-
-
Kurdila, A.J.1
Webb, G.2
-
15
-
-
0032274672
-
Hysteresis modeling of SMA actuators for control actuations
-
Kurdila, A. J., Webb, G., and Lagoudas, D. L. (1998). "Hysteresis modeling of SMA actuators for control actuations." J. Intell. Mater. Syst. Struct., 9(6), 432-448.
-
(1998)
J. Intell. Mater. Syst. Struct.
, vol.9
, Issue.6
, pp. 432-448
-
-
Kurdila, A.J.1
Webb, G.2
Lagoudas, D.L.3
-
16
-
-
11744288552
-
Helicopter vibration reduction with trailing edge flaps
-
American Helicopter Society, Alexandria, Va.
-
Milgram, J., and Chopra, I. (1995) "Helicopter vibration reduction with trailing edge flaps." Proc., American Helicopter Society Northeast Region Aeromechanics Specialists' Meeting, American Helicopter Society, Alexandria, Va.
-
(1995)
Proc., American Helicopter Society Northeast Region Aeromechanics Specialists' Meeting
-
-
Milgram, J.1
Chopra, I.2
-
17
-
-
3042659577
-
Dynamics of an actively controlled plain trailing edge flap system for a modern bearingless rotor
-
Dresden, Germany
-
Milgram, J., and Chopra, I. (1997). "Dynamics of an actively controlled plain trailing edge flap system for a modern bearingless rotor." Proc., 23rd European Rotorcraft Forum, Dresden, Germany.
-
(1997)
Proc., 23rd European Rotorcraft Forum
-
-
Milgram, J.1
Chopra, I.2
-
18
-
-
0004974797
-
Vibration reduction in helicopter rotors using an active control surface located on the blade
-
American Institute of Aeronautics and Astronautics, Washington, D.C.
-
Millot, T. A., and Friedmann, P. P. (1992). "Vibration reduction in helicopter rotors using an active control surface located on the blade." Proc., 33rd Structures, Structural Dynamics, and Materials Confer ence, American Institute of Aeronautics and Astronautics, Washington, D.C., 1975-1988.
-
(1992)
Proc., 33rd Structures, Structural Dynamics, and Materials Confer Ence
, pp. 1975-1988
-
-
Millot, T.A.1
Friedmann, P.P.2
-
19
-
-
0003337825
-
Vibration reduction in helicopter rotors using an actively controlled partial span trailing edge flap located on the blade
-
National Aeronautics and Space Administration, Washington, D.C.
-
Millot, T. A., and Friedmann, P. P. (1994a). "Vibration reduction in helicopter rotors using an actively controlled partial span trailing edge flap located on the blade." NASA CR 4611, National Aeronautics and Space Administration, Washington, D.C.
-
(1994)
NASA CR
, vol.4611
-
-
Millot, T.A.1
Friedmann, P.P.2
-
20
-
-
0003337825
-
Vibration reduction in helicopter rotors using an actively controlled partial span trailing edge flap located on the blade
-
National Aeronautics and Space Administration, Washington, D.C.
-
Millot, T. A., and Friedmann, P. P. (1994b). "Vibration reduction in helicopter rotors using an actively controlled partial span trailing edge flap located on the blade." NASA Contractor Rep. 4611, National Aeronautics and Space Administration, Washington, D.C.
-
(1994)
NASA Contractor Rep.
, vol.4611
-
-
Millot, T.A.1
Friedmann, P.P.2
-
22
-
-
0025258095
-
Piezoelectric actuators for helicopter rotor control
-
American Institute of Aeronautics and Astronautics, Washington, D.C.
-
Spangler, R. L., and Hall, S. R. (1990). "Piezoelectric actuators for helicopter rotor control." Proc., 31st Structures, Structural Dynamics, and Materials Conference, American Institute of Aeronautics and Astronautics, Washington, D.C.
-
(1990)
Proc., 31st Structures, Structural Dynamics, and Materials Conference
-
-
Spangler, R.L.1
Hall, S.R.2
-
23
-
-
0003248504
-
Smart materials for helicopter rotor active control
-
Advisory Group for Aerospace Research and Development, Geneva
-
Strehlow, H., and Rapp, H. (1992). "Smart materials for helicopter rotor active control." Proc., AGARD/SMP Specialist's Meeting on Smart Structures for Aircraft and Spacecraft, Advisory Group for Aerospace Research and Development, Geneva.
-
(1992)
Proc., AGARD/SMP Specialist's Meeting on Smart Structures for Aircraft and Spacecraft
-
-
Strehlow, H.1
Rapp, H.2
-
26
-
-
0002332181
-
Design and testing of helicopter rotor model with smart trailing edge flaps
-
American Institute of Aeronautics and Astronautics, Washington, D.C.
-
Walz, C., and Chopra, I. (1994). "Design and testing of helicopter rotor model with smart trailing edge flaps." Proc., 35th Structures, Structural Dynamics, and Materials Conference, Adaptive Structures Forum, American Institute of Aeronautics and Astronautics, Washington, D.C.
-
(1994)
Proc., 35th Structures, Structural Dynamics, and Materials Conference, Adaptive Structures Forum
-
-
Walz, C.1
Chopra, I.2
-
27
-
-
0031379842
-
Nonlinear electronic control of an electrostrictive actuator
-
International Society for Optical Engineering, Bellingham, Wash.
-
Zvonar, G. A., and Lindner, D. K. (1997). "Nonlinear electronic control of an electrostrictive actuator." Proc., 1997 North American Symposium on Smart Structures and Materials: Industrial and Commercial Applications of Smart Structures Technologies, International Society for Optical Engineering, Bellingham, Wash., 448-458.
-
(1997)
Proc., 1997 North American Symposium on Smart Structures and Materials: Industrial and Commercial Applications of Smart Structures Technologies
, pp. 448-458
-
-
Zvonar, G.A.1
Lindner, D.K.2
|