10.1109/CDC.2007.4434213Proceedings of the IEEE Conference on Decision and Control1963-1968PCDC
International audienceThis paper presents the design and evaluation of a nonlinear control scheme fo...
In this paper, we compare three different control methodologies for helicopter autopilot design: lin...
We consider the problem of controlling the vertical, lateral and longitudinal motion of a nonlinear ...
10.1109/TIE.2008.926780IEEE Transactions on Industrial Electronics5593426-3434ITIE
SIGLEAvailable from British Library Document Supply Centre-DSC:DX192472 / BLDSC - British Library Do...
10.1109/CHICC.2006.2809222006 Chinese Control Conference Proceedings, CCC 20062087-209
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
Nonlinear control laws often need be implemented with digital hardware. Use of digital control syste...
This paper discusses the yaw control of small-size unmanned helicopter. The yaw dynamics of helicopt...
本文着重解决小型无人直升机航向自适应控制问题.通过求非线性函数导数,把原始系统扩展为一个带有伪状态变量的新系统.这种方法不必求解非线性函数的逆,并且降低了计算量.证明了该方法的稳定性.针对实际模型直升...
M.Ing.Linear control system theory is well developed and has lead to a number of control system type...
Abstract: The paper addresses the design of an autopilot for small scale helicopters to let the vert...
This paper studies the multi-source disturbances attenuation problem on the yaw motion of unmanned a...
10.1109/CHICC.2006.4347398Proceedings of the 26th Chinese Control Conference, CCC 2007662-66
An enhanced data driven model-free adaptive yaw control tracking control scheme is proposed for the ...
International audienceThis paper presents the design and evaluation of a nonlinear control scheme fo...
In this paper, we compare three different control methodologies for helicopter autopilot design: lin...
We consider the problem of controlling the vertical, lateral and longitudinal motion of a nonlinear ...
10.1109/TIE.2008.926780IEEE Transactions on Industrial Electronics5593426-3434ITIE
SIGLEAvailable from British Library Document Supply Centre-DSC:DX192472 / BLDSC - British Library Do...
10.1109/CHICC.2006.2809222006 Chinese Control Conference Proceedings, CCC 20062087-209
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
Nonlinear control laws often need be implemented with digital hardware. Use of digital control syste...
This paper discusses the yaw control of small-size unmanned helicopter. The yaw dynamics of helicopt...
本文着重解决小型无人直升机航向自适应控制问题.通过求非线性函数导数,把原始系统扩展为一个带有伪状态变量的新系统.这种方法不必求解非线性函数的逆,并且降低了计算量.证明了该方法的稳定性.针对实际模型直升...
M.Ing.Linear control system theory is well developed and has lead to a number of control system type...
Abstract: The paper addresses the design of an autopilot for small scale helicopters to let the vert...
This paper studies the multi-source disturbances attenuation problem on the yaw motion of unmanned a...
10.1109/CHICC.2006.4347398Proceedings of the 26th Chinese Control Conference, CCC 2007662-66
An enhanced data driven model-free adaptive yaw control tracking control scheme is proposed for the ...
International audienceThis paper presents the design and evaluation of a nonlinear control scheme fo...
In this paper, we compare three different control methodologies for helicopter autopilot design: lin...
We consider the problem of controlling the vertical, lateral and longitudinal motion of a nonlinear ...
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