Real-Time Integral Backstepping with Sliding Mode Control for a Quadrotor UAV
نویسندگان
چکیده
منابع مشابه
Adaptive Sliding Backstepping Control of Quadrotor UAV Attitude
This paper proposes an adaptive sliding backstepping control law for quadcopter attitude control. By employing adaptive elements in the sliding mode control formulation the proposed control law avoids a priori knowledge of the upper bounds on the uncertainty. The controller we propose can be used for systems that are in strict feedback form with matched uncertainties. Numerical simulations show...
متن کاملSliding Mode Control Based on Backstepping Approach for an UAV Type-Quadrotor
In this paper; we are interested principally in dynamic modelling of quadrotor while taking into account the high-order nonholonomic constraints in order to develop a new control scheme as well as the various physical phenomena, which can influence the dynamics of a flying structure. These permit us to introduce a new state-space representation. After, the use of Backstepping approach for the s...
متن کاملComparison of Quadrotor Performance Using Backstepping and Sliding Mode Control
A quadrotor is nonlinear, coupled and unstable system. Two control schemes, namely backstepping and sliding mode, have been applied to obtain desired trajectory tracking by quadrotor. This paper presents the comparative performance results of quadrotor under two control schemes.
متن کاملOptimal Integral Sliding Mode Controller of a UAV With Considering Actuator Fault
In this paper, using the State Dependent Riccati Equation (SDRE) method, we propose a Robust Optimal Integral Sliding Mode Controller (ROISMC) to guarantee an optimal control law for a quadrotor which has become increasingly important by virtue of its high degrees of manoeuvres ability in presence of unknown time-varying external disturbances and actuator fault. The robustness of the controller...
متن کاملRobust Chattering Free Backstepping Sliding Mode Control Strategy for Autonomous Quadrotor Helicopter
Abstract— In this paper a robust chattering free backstepping sliding mode controller is developed for the attitude stabilization and trajectory tracking control of quadrotor helicopter with external disturbances. The control scheme is developed based on backstepping technique and a sliding surface is introduced in the final stage of the algorithm. To attenuate the chattering problem caused by ...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: IFAC-PapersOnLine
سال: 2018
ISSN: 2405-8963
DOI: 10.1016/j.ifacol.2018.07.337