-
1
-
-
33846133856
-
Flight testing of a reconfigurable flight control law on the X-36 tailless fighter aircraft
-
AIAA-2000-3941
-
Brinker J S, Wise K A. Flight testing of a reconfigurable flight control law on the X-36 tailless fighter aircraft[R]. AIAA-2000-3941, 2000
-
(2000)
-
-
Brinker, J.S.1
Wise, K.A.2
-
2
-
-
29744448748
-
Control law reconfiguration using robust linear parameter varying control
-
AIAA-99-4137
-
Bennani S, Sluis R, Schram G, et al. Control law reconfiguration using robust linear parameter varying control[R]. AIAA-99-4137, 1999
-
(1999)
-
-
Bennani, S.1
Sluis, R.2
Schram, G.3
-
3
-
-
85085776091
-
Robust fault-tolerant control design for aircraft under state-dependent disturbances
-
AIAA 2003-5490
-
Boskovic J D, Mehra R K. Robust fault-tolerant control design for aircraft under state-dependent disturbances[R]. AIAA 2003-5490, 2003
-
(2003)
-
-
Boskovic, J.D.1
Mehra, R.K.2
-
4
-
-
0035335741
-
Two reconfigurable flight-control design methods: Robust servomechanism and control allocation
-
Burken J J, Lu P, Wu Z L, et al. Two reconfigurable flight-control design methods: robust servomechanism and control allocation[J]. Journal of Guidance, Control and Dynamics, 2001, 24(3): 482-493
-
(2001)
Journal of Guidance, Control and Dynamics
, vol.24
, Issue.3
, pp. 482-493
-
-
Burken, J.J.1
Lu, P.2
Wu, Z.L.3
-
5
-
-
72449187753
-
Computationally efficient use of MPC and dynamic inversion for reconfigurable flight control
-
AIAA 2008-7431
-
Joosten D A, Boom T J J, Lombaerts T J J. Computationally efficient use of MPC and dynamic inversion for reconfigurable flight control[R]. AIAA 2008-7431, 2008
-
(2008)
-
-
Joosten, D.A.1
Boom, T.J.J.2
Lombaerts, T.J.J.3
-
6
-
-
0003934537
-
Nonlinear tracking and decoupling by trajectory linearization
-
NASA Marshall Space Flight Center
-
Zhu J J. Nonlinear tracking and decoupling by trajectory linearization[R]. NASA Marshall Space Flight Center, 1998
-
(1998)
-
-
Zhu, J.J.1
-
7
-
-
72449121125
-
Improved trajectory linearization flight controller for reusable launch vehicles
-
AIAA 2004-875
-
Bevacqua T, Best E, Huizenga A, et al. Improved trajectory linearization flight controller for reusable launch vehicles[R]. AIAA 2004-875, 2004
-
(2004)
-
-
Bevacqua, T.1
Best, E.2
Huizenga, A.3
-
8
-
-
0031347874
-
PD-spectral theory for multivariable linear time-varying systems
-
Peshkin M., San Diego: IEEE Control Systems Society
-
Zhu J J. PD-spectral theory for multivariable linear time-varying systems[C]//Peshkin M. Proceeding of the 36th Conference on Decision & Control. San Diego: IEEE Control Systems Society, 1997: 3908-3913
-
(1997)
Proceeding of the 36th Conference on Decision & Control
, pp. 3908-3913
-
-
Zhu, J.J.1
-
9
-
-
34547332971
-
A new optimal control allocation method for aircraft with multiple control effectors
-
AIAA 2007-1052
-
Yang Lingyu, Shen Gongzhang. A new optimal control allocation method for aircraft with multiple control effectors[R]. AIAA 2007-1052, 2007
-
(2007)
-
-
Yang, L.1
Shen, G.2
-
10
-
-
37749043711
-
The nonlinear iterative closed loop configuration of control allocation for aircraft with multiple control effectors
-
Cheng D. and Wu M., Beijing: Beijing University of Aeronautics and Astronautics Press, in Chinese
-
Yang Lingyu, Zhong Youwu, Shen Gongzhang. The nonlinear iterative closed loop configuration of control allocation for aircraft with multiple control effectors[C]//Cheng Daizhan, Wu Min. Proceeding of the 26th Chinese Control Conference (Volume 4). Beijing: Beijing University of Aeronautics and Astronautics Press, 2007: 755-757 (in Chinese)
-
(2007)
Proceeding of the 26th Chinese Control Conference (Volume 4)
, vol.4
, pp. 755-757
-
-
Yang, L.1
Zhong, Y.2
Shen, G.3
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