2013
DOI: 10.1007/s11071-013-1099-x
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Airship horizontal trajectory tracking control based on Active Disturbance Rejection Control (ADRC)

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Cited by 139 publications
(70 citation statements)
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“…(6) where A aw = A + B 2 (I − L) −1 K, B aw = B 2 (I − L) −1 , C aw = (I − L) −1 C 2 , D aw = (I − L) −1 D 22 , K and L are parameters of anti-windup compensator which will be solved later; the outputs of MRAW compensator are y aw and v aw ; and sat(µ) represents the control variable saturation:…”
Section: Design Of Model Recovery Anti-windup Compensatormentioning
confidence: 99%
See 1 more Smart Citation
“…(6) where A aw = A + B 2 (I − L) −1 K, B aw = B 2 (I − L) −1 , C aw = (I − L) −1 C 2 , D aw = (I − L) −1 D 22 , K and L are parameters of anti-windup compensator which will be solved later; the outputs of MRAW compensator are y aw and v aw ; and sat(µ) represents the control variable saturation:…”
Section: Design Of Model Recovery Anti-windup Compensatormentioning
confidence: 99%
“…To realize disturbance rejection, an active disturbance rejection control algorithm is designed for airship horizontal model in literature [6]. A method to design an optimal disturbance rejection PID controller is presented in literature [7].…”
Section: Introductionmentioning
confidence: 99%
“…Moreover, ADRC has already demonstrated its effectiveness in many fields. [20][21][22][23][24][25][26][27][28][29][30][31] In this paper, the intrinsic characteristics of the flight mechanics are well utilized to design a novel feed-forwardfeedback control framework such that high flight path control performance can be achieved for hypersonic flight. The feedforward channel feeds the flight path reference straightforwardly to the pitch control loop where the major control component can be generated in an efficient way.…”
Section: Introductionmentioning
confidence: 99%
“…Furthermore, dynamic inversion technology [13,14] and backstepping technology [15,16] have been applied to the autonomous airship based on its nonlinear model. In addition to stabilization control, the trajectory tracking [17,18] and pathfollowing control [19] driving the position of airship to a desired time-varying trajectory should be studied, and the airship can be controlled to perform the cruising flight [20][21][22] and station-keeping tasks [23][24][25]. For the cruising flight task, a straight-line trajectory can be designed, and the trajectory tracking controller achieves line tracking to perform the monitoring and transporting applications simultaneously.…”
Section: Introductionmentioning
confidence: 99%