某型飞机采用DCCIP方式投放炸弹的精度分析

分析了影响DCCIP攻击方式轰炸精度的各种误差源,针对某型飞机平显火控系统的不同组合方式,建立了相应的精度分析数学模型,采用定型试飞数据,仿真计算了各种组合方式下的水平DCCIP轰炸精度.仿真计算结果与定型靶试数据吻合,在某型飞机平显火控系统的靶试的定型中得到了实际应用.     

自治式潜水器规避航行神经网络控制器设计

在规避机动状态下,为了实现对自治式潜水器良好的航行控制,通过分析潜水器的运动状态,建立了运动状态方程,确立了非线性单输入/单输出系统.同时,将复杂的非线性模型通过微分同胚的方法转化为降阶的线性模型,并在此基础上提出了一种基于神经网络的控制方法:将滑模控制思想、反馈线性化理论及神经网络在线建模方法相结合,提出了基于神经网络的鲁棒自适应控制算法,并将此方法用于自治式潜水器高度保持的仿真中,从仿真的结果来看,控制器具有满意的控制效果,证实了该方法的有效性,能为自治式潜水器航行控制提供一定的参考.     

离散变结构控制系统的变速趋近律

首次提出了离散变结构控制的变速趋近律．文中指出,在变速趋近律的制约下,会出现扇形的切换区．给出了扇形切换区准滑动模态的数学模型．     

装备维修器材竞争性采购方式的模糊决策

针对传统装备维修器材采购方式选择主观性强、不规范等问题,通过选取“保密性、安全性、市场性、时间性和经济性”5条指标,借用层次分析法和模糊综合决策,建立了采购方式选择的量化模型,利用可调整的评语集,优化了模型决策过程,实现了采购方式选择的快速决策．     

基本作战样式下航母编队兵力配置方法

航母编队兵力配置是航母编队作战运用的基础内容,从作战任务的角度来研究航母编队兵力配置问题。航母编队基本作战样式可分为对空作战、对海作战、对潜作战和对岸作战4种,航母编队通过基本作战样式的组合来达成作战任务。基于每种作战样式下航母编队兵力执行的作战任务,确定了兵力配置的原则和方法。为研究航母编队兵力配置问题提供了一种可借鉴的思路。     

不同导引模式下的末修弹脉冲参数优化研究

在总脉冲量确定的情形下,在启控时间、总脉冲数、最小点火时间间隔及点火阈值等脉冲参数对末修弹落点散布的影响进行详细分析的基础上,利用数值仿真的方法,对比例导引模式、抛物线导引模式、落点预测导引模式、弹道追踪导引模式和zx导引模式等常用导引模式下的脉冲参数优化进行深入分析研究．     

基于中间件技术的FGIS与PGIS对接实现技术研究

利用中间件技术,在不影响现有消防地理信息系统应用的前提下,充分共享警用地理信息系统（PGIS）已有建设成果,实现在消防地理信息系统（FGIS）中调用PGIS大比例尺矢量图等信息数据资源,降低了FGIS建设成本,减轻了业务数据采集、维护压力.并对基于中间件技术的数据对接设计思路、整体架构进行了详细阐述.     

基于协同交战的战术数据链技术研究

介绍了外军典型战术数据链的发展情况,同时根据未来网络化作战需求,对基于协同交战的战术数据链的作战使用进行了研究,提出了基于协同交战的战术数据链体系结构、功能需求和指标需求,最后给出了基于协同交战的战术数据链的发展建议.     

Dual-steering mode based on direct yaw moment control for multi-wheel hub motor driven vehicles:Theoretical design and experimental assessment

One of the main challenges for multi-wheel hub motor driven vehicles is the coordination of individual drivetrains to improve mobility and stability in the steering process.This paper proposes a dual-steering mode based on direct yaw moment control for enhancing vehicle steering ability in complex environ-ments.The control system is designed as a hierarchical structure,with a yaw moment decision layer and a driving force distribution layer.In the higher-level layer,the objective optimization function is con-structed to obtain the slip steering ratio,which represents the degree of vehicle slip steering in the dual-steering mode.A yaw moment controller using active disturbance rejection control theory is designed for continuous yaw rate control.When the actual yaw rate of the vehicle deviates from the reference yaw rate obtained by the vehicle reference model and the slip steering ratio,the yaw moment controller is actuated to determine the yaw moment demand for vehicle steering.In the lower-level layer,there is a torque distribution controller based on distribution rules,which meets the requirement of yaw moment demand without affecting the total longitudinal driving force of the vehicle.For verifying the validity and feasibility of the dual-steering mode,simulations were conducted on the hardware-in-loop real-time simulation platform.Additionally,corresponding real vehicle tests were carried out on an eight-wheel prototype vehicle.Test results were generally consistent with the simulation results,thereby demon-strating that the proposed dual-steering mode reduces steering radius and enhances the steering per-formance of the vehicle.     

Adaptive sliding mode control of modular self-reconfigurable spacecraft with time-delay estimation

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.