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Adaptive Predefined-Time Attitude Tracking Control for Quadrotor Using a Novel Terminal Sliding Mode Approach
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作者 Tianshuo Ge Tengshuo Dong +1 位作者 Baihai Zhang Fenxi Yao 《Journal of Beijing Institute of Technology》 EI CAS 2024年第6期530-546,共17页
This paper proposes an adaptive predefined-time terminal sliding mode control(APTSMC)scheme for attitude tracking control of a quadrotor.To create this,an adaptive predefined-time stability controller based on a termi... This paper proposes an adaptive predefined-time terminal sliding mode control(APTSMC)scheme for attitude tracking control of a quadrotor.To create this,an adaptive predefined-time stability controller based on a terminal sliding mode is constructed.The upper bound of convergence time in the proposed scheme can be adjusted by the explicit parameters during the design process of the controller.In addition,it is proved that the attitude tracking error will converge within two periods of the preset time.These two periods are set between two ranges:From the initial values to the sliding mode surface and from the sliding mode surface to the region near the origin.Furthermore,an adaptive law is adopted to eliminate unknown external disturbances and the effects of the uncertainties in the quadrotor model,so it is unnecessary to require the prior knowledge of the upper bound of the perturbations.Simulation results are produced and comparative case studies are carried out to demonstrate that the proposed scheme has faster convergence speed and smaller tracking errors. 展开更多
关键词 predefined-time QUADROTOR attitude tracking control adaptive terminal sliding mode
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Adaptive Super‑Twisting Sliding Mode Fault‑Tolerant Control of Launch Vehicles with Actuator Faults
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作者 WANG Kejun ZHOU Zhijie +3 位作者 FENG Zhichao YANG Ruohan HU Changhua XU Hui 《Transactions of Nanjing University of Aeronautics and Astronautics》 CSCD 2024年第6期689-699,共11页
A fault-tolerant control law based on adaptive super-twisting sliding mode control(SMC)is designed for the attitude command tracking problem of a launch vehicle with actuator faults,considering the uncertainties arisi... A fault-tolerant control law based on adaptive super-twisting sliding mode control(SMC)is designed for the attitude command tracking problem of a launch vehicle with actuator faults,considering the uncertainties arising from unknown external disturbances,fuel consumption of the launch vehicle,and the perturbation due to the change in rotational inertia caused by tank sloshing,as well as the potential system model changes due to actuator fault and unmodeled dynamics.This control algorithm integrates the super-twisting SMC,the fuzzy logic control,and the adaptive control.First,a super-twisting sliding surface is selected to mitigate the“chattering”phenomenon inherent in SMC,ensuring that the system tracking error converges to zero within a finite time.Second,building upon this sliding surface,the fuzzy logic control is used to approximate the unknown system function,which includes fault information.Adaptive parameters are used to approach the system parameters and enhance disturbance rejection.The stability and finite-time convergence of the launch vehicle attitude tracking control system are verified by the Lyapunov method.Numerical simulations demonstrate the effectiveness and robustness of the proposed adaptive super-twisting SMC algorithm. 展开更多
关键词 launch vehicle actuator fault super-twisting sliding mode control(SMC) fault-tolerant control fuzzy logic control
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Generalized projective synchronization of the fractional-order chaotic system using adaptive fuzzy sliding mode control 被引量:3
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作者 王立明 唐永光 +1 位作者 柴永泉 吴峰 《Chinese Physics B》 SCIE EI CAS CSCD 2014年第10期64-70,共7页
An adaptive fuzzy sliding mode strategy is developed for the generalized projective synchronization of a fractional- order chaotic system, where the slave system is not necessarily known in advance. Based on the desig... An adaptive fuzzy sliding mode strategy is developed for the generalized projective synchronization of a fractional- order chaotic system, where the slave system is not necessarily known in advance. Based on the designed adaptive update laws and the linear feedback method, the adaptive fuzzy sliding controllers are proposed via the fuzzy design, and the strength of the designed controllers can he adaptively adjusted according to the external disturbances. Based on the Lya- punov stability theorem, the stability and the robustness of the controlled system are proved theoretically. Numerical simu- lations further support the theoretical results of the paper and demonstrate the efficiency of the proposed method. Moreover, it is revealed that the proposed method allows us to manipulate arbitrarily the response dynamics of the slave system by adjusting the desired scaling factor λi and the desired translating factor ηi, which may be used in a channel-independent chaotic secure communication. 展开更多
关键词 generalized projective chaos synchronization fuzzy sliding mode control fractional order chaoticsystem
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ROBUST ADAPTIVE SLIDING MODE CONTROL FOR NONLINEAR UNCERTAIN NEUTRAL DELAY SYSTEM 被引量:2
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作者 王岩青 姜长生 陈海通 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2005年第3期259-263,共5页
Robust stabilization for a class of nonlinear uncertain neutral system with time-varying delay is investigated. By applying the Lyapunov stability theorem, an adaptive sliding mode controller (ADSMC) is developed.Ba... Robust stabilization for a class of nonlinear uncertain neutral system with time-varying delay is investigated. By applying the Lyapunov stability theorem, an adaptive sliding mode controller (ADSMC) is developed.Based on the sliding mode control technique, the controller can drive the system into a pre-specified sliding hyperplane to obtain the desired dynamic performance. Once the system dynamics reaches the sliding plane, the control system is insensitive to uncertainty. The adaptive technique can overcome the unknown upper bound of uncertainty so that the reaching condition can be satisfied. Furthermore, the controller does not include any delayed state,so such an ADSMC is memoryless. Finally, a numerical example is given to verify the validity of the developed memoryless ADSMC and the globally asymptotic stability is guaranteed for the control scheme. 展开更多
关键词 neutral delay system robust control adaptATION sliding mode control
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Dynamic analysis and fractional-order adaptive sliding mode control for a novel fractional-order ferroresonance system 被引量:1
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作者 杨宁宁 韩宇超 +2 位作者 吴朝俊 贾嵘 刘崇新 《Chinese Physics B》 SCIE EI CAS CSCD 2017年第8期74-86,共13页
Ferroresonance is a complex nonlinear electrotechnical phenomenon, which can result in thermal and electrical stresses on the electric power system equipments due to the over voltages and over currents it generates. T... Ferroresonance is a complex nonlinear electrotechnical phenomenon, which can result in thermal and electrical stresses on the electric power system equipments due to the over voltages and over currents it generates. The prediction or determination of ferroresonance depends mainly on the accuracy of the model used. Fractional-order models are more accurate than the integer-order models. In this paper, a fractional-order ferroresonance model is proposed. The influence of the order on the dynamic behaviors of this fractional-order system under different parameters n and F is investigated. Compared with the integral-order ferroresonance system, small change of the order not only affects the dynamic behavior of the system, but also significantly affects the harmonic components of the system. Then the fractional-order ferroresonance system is implemented by nonlinear circuit emulator. Finally, a fractional-order adaptive sliding mode control (FASMC) method is used to eliminate the abnormal operation state of power system. Since the introduction of the fractional-order sliding mode surface and the adaptive factor, the robustness and disturbance rejection of the controlled system are en- hanced. Numerical simulation results demonstrate that the proposed FASMC controller works well for suppression of ferroresonance over voltage. 展开更多
关键词 fractional-order ferroresonance system fractional-order sliding mode control adaptive control nonlinear circuit emulator
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Adaptive sliding mode control of modular self-reconfigurable spacecraft with time-delay estimation 被引量:1
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作者 Xin-hong Li Zhi-bin Zhang +4 位作者 Ji-ping An Xin Zhou Gang-xuan Hu Guo-hui Zhang Wan-xin Man 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2022年第12期2170-2180,共11页
The reconstruction control of modular self-reconfigurable spacecraft (MSRS) is addressed using an adaptive sliding mode control (ASMC) scheme based on time-delay estimation (TDE) technology. In contrast to the ground,... The reconstruction control of modular self-reconfigurable spacecraft (MSRS) is addressed using an adaptive sliding mode control (ASMC) scheme based on time-delay estimation (TDE) technology. In contrast to the ground, the base of the MSRS is floating when assembled in orbit, resulting in a strong dynamic coupling effect. A TED-based ASMC technique with exponential reaching law is designed to achieve high-precision coordinated control between the spacecraft base and the robotic arm. TDE technology is used by the controller to compensate for coupling terms and uncertainties, while ASMC can augment and improve TDE’s robustness. To suppress TDE errors and eliminate chattering, a new adaptive law is created to modify gain parameters online, ensuring quick dynamic response and high tracking accuracy. The Lyapunov approach shows that the tracking errors are uniformly ultimately bounded (UUB). Finally, the on-orbit assembly process of MSRS is simulated to validate the efficacy of the proposed control scheme. The simulation results show that the proposed control method can accurately complete the target module’s on-orbit assembly, with minimal perturbations to the spacecraft’s attitude. Meanwhile, it has a high level of robustness and can effectively eliminate chattering. 展开更多
关键词 adaptive sliding mode control(ASMC) Time delay control Time delay estimation Modular self-reconfigurable spacecraft Uncertainty Coordinated control
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Application of Adaptive Backstepping Sliding Mode Control in Alternative Current Servo System of Rocket Launcher
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作者 郭亚军 马大为 +1 位作者 王晓峰 乐贵高 《Defence Technology(防务技术)》 SCIE EI CAS 2011年第3期140-144,共5页
An adaptive backstepping sliding mode control approach is introduced to control the pitch motion of a rocket launcher. Its control law is proposed to guarantee that the control system is ultimately bounded in a Lyapun... An adaptive backstepping sliding mode control approach is introduced to control the pitch motion of a rocket launcher. Its control law is proposed to guarantee that the control system is ultimately bounded in a Lyapunov sense and make the servo system track the instruction of reference position globally and asymptotically. In addition, the sliding mode control can restrain the effects of parameter uncertainties and external disturbance. The functions of adaptive mechanism and sliding mode control are analyzed through the simulation in the different conditions.The simulation results illustrate that the method is applicable and robust. 展开更多
关键词 automatic control technology rocket launcher sliding mode control adaptive backstepping permanent magnet synchronous motor
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FUZZY ADAPTIVE CONTROL OF FLEXIBLE-LINK ROBOT MANIPULATOR 被引量:1
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作者 倪受东 吴洪涛 +1 位作者 袁祖强 嵇海平 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2004年第3期200-205,共6页
A fuzzy adaptive control method is proposed for a flexible robot manipulator. Due to the structure characteristics of the flexible manipulator, the vibration modes must be controlled to realize the high-precision tip ... A fuzzy adaptive control method is proposed for a flexible robot manipulator. Due to the structure characteristics of the flexible manipulator, the vibration modes must be controlled to realize the high-precision tip position. The Lagrangian principle is utilized to model the dynamic function of the single-degree flexible manipulator incorporating the assumed modes method. Simulation results of the fuzzy adaptive control method in the location control and the trajectory tracking with different tip disturbances are presented and compared with the results of the classic PD control. It shows that the controller can obtain the stable and robust performance. 展开更多
关键词 flexible robot manipulator Lagrangian function assumed mode method fuzzy adaptive control
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Full-order sliding mode control of uncertain chaos in a permanent magnet synchronous motor based on a fuzzy extended state observer 被引量:9
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作者 陈强 南余荣 +1 位作者 郑恒火 任雪梅 《Chinese Physics B》 SCIE EI CAS CSCD 2015年第11期157-162,共6页
A full-order sliding mode control based on a fuzzy extended state observer is proposed to control the uncertain chaos in the permanent magnet synchronous motor. Through a simple coordinate transformation, the chaotic ... A full-order sliding mode control based on a fuzzy extended state observer is proposed to control the uncertain chaos in the permanent magnet synchronous motor. Through a simple coordinate transformation, the chaotic PMSM model is transformed into the Brunovsky canonical form, which is more suitable for the controller design. Based on the fuzzy control theory, a fuzzy extended state observer is developed to estimate the unknown states and uncertainties, and the restriction that all the system states should be completely measurable is avoided. Thereafter, a full-order sliding mode controller is designed to ensure the convergence of all system states without any chattering problem. Comparative simulations show the effectiveness and superior performance of the proposed control method. 展开更多
关键词 permanent magnet synchronous motor chaotic system sliding mode control fuzzy extended stateobserver
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Integrated guidance and control of guided projectile with multiple constraints based on fuzzy adaptive and dynamic surface 被引量:6
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作者 Shang Jiang Fu-qing Tian +1 位作者 Shi-yan Sun Wei-ge Liang 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2020年第6期1130-1141,共12页
Based on fuzzy adaptive and dynamic surface(FADS),an integrated guidance and control(IGC)approach was proposed for large caliber naval gun guided projectile,which was robust to target maneuver,canard dynamic character... Based on fuzzy adaptive and dynamic surface(FADS),an integrated guidance and control(IGC)approach was proposed for large caliber naval gun guided projectile,which was robust to target maneuver,canard dynamic characteristics,and multiple constraints,such as impact angle,limited measurement of line of sight(LOS)angle rate and nonlinear saturation of canard deflection.Initially,a strict feedback cascade model of IGC in longitudinal plane was established,and extended state observer(ESO)was designed to estimate LOS angle rate and uncertain disturbances with unknown boundary inside and outside of system,including aerodynamic parameters perturbation,target maneuver and model errors.Secondly,aiming at zeroing LOS angle tracking error and LOS angle rate in finite time,a nonsingular terminal sliding mode(NTSM)was designed with adaptive exponential reaching law.Furthermore,combining with dynamic surface,which prevented the complex differential of virtual control laws,the fuzzy adaptive systems were designed to approximate observation errors of uncertain disturbances and to reduce chatter of control law.Finally,the adaptive Nussbaum gain function was introduced to compensate nonlinear saturation of canard deflection.The LOS angle tracking error and LOS angle rate were convergent in finite time and whole system states were uniform ultimately bounded,rigorously proven by Lyapunov stability theory.Hardware-in-the-loop simulation(HILS)and digital simulation experiments both showed FADS provided guided projectile with good guidance performance while striking targets with different maneuvering forms. 展开更多
关键词 Integrated guidance and control Multiple constraints fuzzy adaptive Dynamic surface Nonsingular terminal sliding mode Extended state observer
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Simulation and Design of Fuzzy Sliding-mode Controller for Ship Heading-tracking 被引量:3
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作者 袁雷 吴汉松 《Journal of Marine Science and Application》 2011年第1期76-81,共6页
In considering the characteristic of a rudder,the maneuvers of a ship were described by an unmatched uncertain nonlinear mathematic model with unknown virtual control coefficient and parameter uncertainties.In order t... In considering the characteristic of a rudder,the maneuvers of a ship were described by an unmatched uncertain nonlinear mathematic model with unknown virtual control coefficient and parameter uncertainties.In order to solve the uncertainties in the ship heading control,specifically the controller singular and paramount re-estimation problem,a new multiple sliding-mode adaptive fuzzy control algorithm was proposed by combining Nussbaum gain technology,the approximation property of fuzzy logic systems,and a multiple sliding-mode control algorithm.Based on the Lyapunov function,it was proven in theory that the controller made all signals in the nonlinear system of unmatched uncertain ship motion uniformly bounded,with tracking errors converging to zero.Simulation results show that the demonstrated controller design can track a desired course fast and accurately.It also exhibits strong robustness peculiarity in relation to system uncertainties and disturbances. 展开更多
关键词 ship autopilot nonlinear system unmatched uncertainty multiple sliding mode control fuzzy control
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Robust fuzzy sliding-mode control for T-S model based permanent magnet synchronous motor
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作者 张细政 王耀南 《中南大学学报(自然科学版)》 EI CAS CSCD 北大核心 2009年第S1期68-73,共6页
A fuzzy sliding-mode control (FSMC) scheme based on T-S fuzzy models was proposed for the permanent magnet synchronous motor (PMSM) drive system to solve the speed tracking problem. A T-S fuzzy model was firstly forme... A fuzzy sliding-mode control (FSMC) scheme based on T-S fuzzy models was proposed for the permanent magnet synchronous motor (PMSM) drive system to solve the speed tracking problem. A T-S fuzzy model was firstly formed to represent the nonlinear system of PMSM. For converting the tracking control into a stabilization problem, a new control design was proposed to define the internal desired states. Then, the FSMC controller for PMSM system with parameter variation and load disturbance was designed based on the fuzzy model. The performance of the proposed controller was verified by experimental results on PMSM system. The results show that the FSMC scheme can drive the dynamics of PMSM into a designated sliding surface in finite time and guarantee the property of asymptotical stability. The information of upper bound of modeling errors as well as perturbations is not required when using the FSMC controller. 展开更多
关键词 PERMANENT MAGNET SYNCHRONOUS motor (PMSM) uncertain T-S nonlinear systems sliding-mode control fuzzy sliding surfaces linear matrix INEQUALITIES (LMIs)
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Tracking consensus for nonlinear heterogeneous multi-agent systems subject to unknown disturbances via sliding mode control 被引量:1
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作者 张翔 王金环 +1 位作者 杨德东 徐勇 《Chinese Physics B》 SCIE EI CAS CSCD 2017年第7期39-48,共10页
We investigate the tracking control for a class of nonlinear heterogeneous leader-follower multi-agent systems(MAS)with unknown external disturbances. Firstly, the neighbor-based distributed finite-time observers ar... We investigate the tracking control for a class of nonlinear heterogeneous leader-follower multi-agent systems(MAS)with unknown external disturbances. Firstly, the neighbor-based distributed finite-time observers are proposed for the followers to estimate the position and velocity of the leader. Then, two novel distributed adaptive control laws are designed by means of linear sliding mode(LSM) as well as nonsingular terminal sliding mode(NTSM), respectively. One can prove that the tracking consensus can be achieved asymptotically under LSM and the tracking error can converge to a quite small neighborhood of the origin in finite time by NTSM in spite of uncertainties and disturbances. Finally, a simulation example is given to verify the effectiveness of the obtained theoretical results. 展开更多
关键词 multi-agent systems tracking consensus distributed adaptive control sliding mode
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Discrete Sliding Mode Control of an Input-output System with Stochastic Disturbance
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作者 CAI Su-fen ZHANG Zhi-ping YIN Zeng-gang 《Chinese Quarterly Journal of Mathematics》 CSCD 北大核心 2006年第3期423-433,共11页
This paper presents the discrete adaptive sliding mode control of input-output non-minimum phase system in the presence of the stochastic disturbance. The non-minimum phase system can be transformed into a minimum pha... This paper presents the discrete adaptive sliding mode control of input-output non-minimum phase system in the presence of the stochastic disturbance. The non-minimum phase system can be transformed into a minimum phase system by a operator. According to the minimum phase system, the controller and the adaptive algorithm we designed ensures the stability of system and holds that the mean-square deviation from the sliding surface is minimized. 展开更多
关键词 input-output system mean-square deviation the discrete adaptive sliding mode control
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Robust Graded Sliding Mode Tracking Control for Low Speed Spinning Ballistic Missiles
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作者 周军 王志 周凤歧 《Defence Technology(防务技术)》 SCIE EI CAS 2007年第1期15-19,共5页
The nonlinear dynamic model of spinning ballistic missiles is established during the first boosting phase of the missile. Based on the conventional backstepping sliding mode control and the assumption of a two time-sc... The nonlinear dynamic model of spinning ballistic missiles is established during the first boosting phase of the missile. Based on the conventional backstepping sliding mode control and the assumption of a two time-scale separation of missile dynamics, a graded sliding mode controller is designed with two sub-sliding surfaces which have invariability to external disturbances and parameter perturbations, and a matrix which comprises three first order low pass filters is introduced to prevent “explosion of terms”. Owing to the upper bounds of the uncertainties are difficult to obtain in advance, adaptive laws are introduced to estimate the values of the uncertainties in real-time. Eventually, the numerical simulation results given to show the proposed controller can ensure the steady flight of missiles. 展开更多
关键词 低速旋转 弹道导弹 飞行控制 分级滑动模 跟踪控制 鲁棒
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Adaptive projective synchronization of different chaotic systems with nonlinearity inputs
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作者 牛玉军 王兴元 裴炳南 《Chinese Physics B》 SCIE EI CAS CSCD 2012年第3期112-120,共9页
We investigate the projective synchronization of different chaotic systems with nonlinearity inputs. Based on the adaptive technique, sliding mode control method and pole assignment technique, a novel adaptive project... We investigate the projective synchronization of different chaotic systems with nonlinearity inputs. Based on the adaptive technique, sliding mode control method and pole assignment technique, a novel adaptive projective synchro- nization scheme is proposed to ensure the drive system and the response system with nonlinearity inputs can be rapidly synchronized up to the given scaling factor. 展开更多
关键词 projective synchronization adaptive technique sliding mode control nonlinearity input
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攻角约束的敏捷机动自适应滑模控制方法
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作者 张旋 陈升泽 王子晗 《导弹与航天运载技术(中英文)》 北大核心 2025年第1期78-84,共7页
针对航天器大攻角敏捷机动控制问题,基于直接力/气动力复合控制策略,提出攻角约束下航天器自适应滑模姿态控制方法。首先,建立纵向直接力/气动力复合控制模型和侧向喷流干扰模型,通过设计考虑攻角约束的预设性能非线性映射函数,将攻角... 针对航天器大攻角敏捷机动控制问题,基于直接力/气动力复合控制策略,提出攻角约束下航天器自适应滑模姿态控制方法。首先,建立纵向直接力/气动力复合控制模型和侧向喷流干扰模型,通过设计考虑攻角约束的预设性能非线性映射函数,将攻角约束的俯仰通道姿态控制问题转换为无约束的攻角误差调节控制问题;其次,设计攻角误差启发的非线性积分型滑模面,在反演控制框架下,提出侧向喷流干扰自适应估计的积分反演滑模控制方法,保证对侧向喷流干扰上界的在线估计,实现大攻角敏捷精准控制。最后,基于Lyapunov稳定性理论,证明了所设计的闭环控制系统的渐近稳定性。数值仿真表明:所提方法相比经典滑模控制方法,稳态时间缩短了79.16%,超调量减小了24.68%,舵偏能量消耗减小了34.54%。 展开更多
关键词 直接力/气动力 预设性能 自适应滑模 姿态控制 敏捷控制
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不确定四旋翼飞行器系统的滑模鲁棒控制
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作者 于涛 苗志鑫 《弹箭与制导学报》 北大核心 2025年第1期34-44,61,共12页
针对不确定四旋翼飞行器系统的控制问题,提出一种基于自适应一阶滑模干扰估计器和二相组合函数趋近律的滑模鲁棒控制策略。将四旋翼飞行器系统分成2个全驱动子系统和2个欠驱动子系统,并采用适当的滑动面设计方法构造各子系统的滑动面。... 针对不确定四旋翼飞行器系统的控制问题,提出一种基于自适应一阶滑模干扰估计器和二相组合函数趋近律的滑模鲁棒控制策略。将四旋翼飞行器系统分成2个全驱动子系统和2个欠驱动子系统,并采用适当的滑动面设计方法构造各子系统的滑动面。采用一种连续的自适应一阶滑模干扰估计器在线逼近各子系统的不确定性因素,并使用一种能够动态适应滑动面变化的二相组合函数趋近律,依次设计全驱动子系统和欠驱动子系统的滑模控制量。从理论上分析了闭环控制系统的稳定性和控制系统滑动面的收敛时间,仿真测试结果验证了所提出的滑模控制策略的鲁棒控制性能和控制器抖动削弱能力。 展开更多
关键词 四旋翼飞行器 滑模鲁棒控制 二相组合函数趋近律 自适应一阶滑模干扰估计器 抖动削弱
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航天器固定时间姿态饱和控制
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作者 肖超 郭永 +3 位作者 邸富强 王力浩 李爱军 王长青 《宇航学报》 北大核心 2025年第1期141-149,共9页
针对面临未知外部扰动与执行器饱和约束的航天器姿态控制系统,提出了一种鲁棒自适应抗饱和固定时间控制策略,解决了航天器在外部扰动与执行器饱和约束下的姿态跟踪控制问题。首先,基于齐次性理论,设计了一种可在固定时间内收敛到零的非... 针对面临未知外部扰动与执行器饱和约束的航天器姿态控制系统,提出了一种鲁棒自适应抗饱和固定时间控制策略,解决了航天器在外部扰动与执行器饱和约束下的姿态跟踪控制问题。首先,基于齐次性理论,设计了一种可在固定时间内收敛到零的非奇异全阶终端滑模面。然后,结合所提出的滑模面与自适应控制,设计了一种鲁棒自适应抗饱和控制器,可确保航天器系统状态在固定时间内完成对期望指令的跟踪。最后,通过理论分析和数值仿真验证了所提出控制策略的有效性,其可为外部扰动与执行器饱和约束下航天器的姿态跟踪提供高精度控制方法。 展开更多
关键词 航天器姿态控制 执行器饱和 固定时间控制 终端滑模控制 自适应控制
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基于复合非线性反馈-自适应积分滑模的飞机主动侧杆随动控制
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作者 邢皓斌 吴阳明 +3 位作者 郑凯 王晓丽 欧阳权 王志胜 《弹箭与制导学报》 北大核心 2025年第1期1-7,共7页
主动侧杆是飞机飞行姿态调节的关键操纵装置。在飞机自动驾驶模式下,主动侧杆随动功能通过实时跟踪飞机的控制指令,增强飞行员对飞行状态的感知,从而有效提升飞行安全性。然而,系统中的未知干扰力矩会导致主动侧杆随动跟踪精度下降。为... 主动侧杆是飞机飞行姿态调节的关键操纵装置。在飞机自动驾驶模式下,主动侧杆随动功能通过实时跟踪飞机的控制指令,增强飞行员对飞行状态的感知,从而有效提升飞行安全性。然而,系统中的未知干扰力矩会导致主动侧杆随动跟踪精度下降。为了解决这一难题,文中设计了一种基于复合非线性反馈-自适应积分滑模的主动侧杆随动控制方法,在复合非线性反馈控制算法基础上加入积分滑模控制算法。其中,复合非线性反馈控制能有效改善系统的稳态性,自适应积分滑模控制能有效抑制系统未知干扰。实验结果表明,所提出的改进飞机主动侧杆随动控制算法与传统复合非线性反馈控制算法相比,调节时间减小约41%,稳态误差减少了约93.6%。此外,在加入常值扭矩扰动下与传统PID算法相比,改进后的随动控制算法调节时间减少了约79%。改进后的主动侧杆随动控制算法显著提升了系统的控制精度和响应性能,并且具有良好的抗干扰能力。 展开更多
关键词 主动侧杆 随动控制 复合非线性反馈 自适应积分滑模控制
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