2020 Chinese Control and Decision Conference (CCDC) 2020
DOI: 10.1109/ccdc49329.2020.9164469
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Aircraft Trajectory Control with Feedback Linearization for General Nonlinear Systems

Abstract: The feedback linearization method is further developed for the controller design on general nonlinear systems. Through the Lyapunov stability theory, the intractable nonlinear implicit algebraic control equations are effectively solved, and the asymptotically tracking performance is guaranteed. Moreover, it is proved that the controller may be used in an inverse-free version to the set-point control. With this method, a nonlinear aircraft outer-loop trajectory controller is developed. For the concern regarding… Show more

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Cited by 7 publications
(8 citation statements)
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“…The dynamics of each agent are based on the model presented in the work by Anderson and Robbins. 24 Using the feedback linearization law described in the work by Zhang et al, 25 the best choice for the control input (velocity vector) that ensures stability of each agent is considered as in equation (53). Control law (31) is considered with ( K x = [ 0 . 16 1 . 53 6 . 4 ] ) .…”
Section: Simulation Resultsmentioning
confidence: 99%
“…The dynamics of each agent are based on the model presented in the work by Anderson and Robbins. 24 Using the feedback linearization law described in the work by Zhang et al, 25 the best choice for the control input (velocity vector) that ensures stability of each agent is considered as in equation (53). Control law (31) is considered with ( K x = [ 0 . 16 1 . 53 6 . 4 ] ) .…”
Section: Simulation Resultsmentioning
confidence: 99%
“…Therefore, the 3DoF model point mass model seems adequate for formation tracking purposes as requested in [36]. Equation (3) shows the model, in which the three first elements represent the kinematic equations and the following three are related to the dynamic equations as it has been considered in other works [36][37][38][39][40]. It should be emphasized that the fuel consumption dynamics has been neglected here, as it is considered of fixed rate first order dynamic and is independent of kinematics and dynamic variables.…”
Section: Uav Model Dynamics and Control Lawmentioning
confidence: 99%
“…Using the feedback linearization law described in Zhang et al [39], the best choice for the control input (velocity vector) that ensures stability of each agent is considered as in (8).…”
Section: Uav Model Dynamics and Control Lawmentioning
confidence: 99%
“…Linearization means that the nonlinear relation of the system is approximated by linear expression at the operating point of the system [41]. The stronger the nonlinearity of the system, the smaller the approximate range of linearization.…”
Section: B Linearization Of Nonlinear Modelsmentioning
confidence: 99%