思乡病
发表于 2025-3-26 22:48:38
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向宇宙
发表于 2025-3-27 03:56:50
2198-4182 Flight Control for UAVs with External Disturbances.ConsidersThis book studies selected discrete-time flight control schemes for fixed-wing unmanned aerial vehicle (UAV) systems in the presence of system uncertainties, external disturbances and input saturation. The main contributions of this book fo
ADJ
发表于 2025-3-27 08:10:23
Discrete-Time Control for Uncertain UAV System Based on SMDO and NN,ler is designed according to the auxiliary system, the NN-based SMDO, the discrete-time tracking differentiator and the BC technology. In Sect. ., numerical simulation results are given to show the effectiveness of discrete-time flight control scheme, followed by some concluding remarks in Sect. ..
NOCT
发表于 2025-3-27 11:45:07
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harangue
发表于 2025-3-27 15:27:24
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Malcontent
发表于 2025-3-27 19:13:51
Modeling of UAV and Preliminaries,duced. Three kinds of input nonlinearities of control input are given in Sect. ., including input saturation, dead-zone nonlinearity and a nonlinearity satisfying asymmetric saturation and dead-zone input. In Sect. ., some lemmas and definitions are presented, and these lemmas and definitions will b
一个姐姐
发表于 2025-3-27 23:48:47
Discrete-Time BC-Based Methods for Fixed-Wing UAV System,n. Then, the discrete-time SMC is used to realize the attitude control for the fixed-wing UAV system with time-varying disturbance in Sect. ., and the results of simulation are given to illustrate the effectiveness of the discrete-time SMC method, followed by drawing some conclusions in Sect. ..
陶器
发表于 2025-3-28 05:11:46
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Accolade
发表于 2025-3-28 10:06:18
Discrete-Time NN Attitude Tracking Control for UAV System with Disturbance and Input Saturation,t with by using NN approximation principle. Furthermore, in order to suppress the negative influence of external disturbances on the system, a DTDO based on the NN is designed, and the output of DTDO is applied to the design of the controller in Sect. .. Meanwhile, the influence of compensating inpu
Incisor
发表于 2025-3-28 13:06:14
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