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141.
142.
With the continuous advancement of the avionics system, crew members are correspondingly reduced, and Single Pilot Operations(SPO) has attracted widespread attention from scholars.To meet the flight requirements in SPO mode, it is necessary to further strengthen air-ground coordination system integration, but at the same time, there will be some safety issues caused by resource integration, function fusion, and task synthesis. Aimed at the safety problems caused by task synthesis, an efficient d... 相似文献
143.
Cooperative differential games guidance laws for multiple attackers against an active defense target
This paper is concerned with a scenario of multiple attackers trying to intercept a target with active defense. Three types of agents are considered in the guidance: The multiple attackers, the target and the defender, where the attackers aim to pursuit the target from different directions and evade from the defender simultaneously. The guidance engagement is formulated in the framework of a zero-sum two-person differential game between the two opposing teams, such that the measurements on the m... 相似文献
144.
基于足部微惯性测量单元(MIMU)和超宽带测距的协同导航技术是一种解决卫星信号受限环境下单兵自主导航难题的有效途径。根据零速修正辅助的惯性解算特点,建立了一种单兵协同导航模型,协同导航状态为各单兵的位置和航向,系统输入为足部MIMU提供的每步位移和航向增量。将算法与相关文献中提出的两种算法进行了对比分析,该算法的优点是无需对足部惯导模块做任何改动和进行反馈修正,易于工程实现且不损失精度。通过三人协同导航试验分析了算法的性能,数据分析表明协同导航在不同条件下可以不同程度地改善系统的定位性能。 相似文献
145.
《中国航空学报》2023,36(2):241-255
This paper presents a discrete-time attitude control strategy with equi-global practical stabilizability for aligning the attitude of multiple spacecraft to a predesigned configuration according to a time-variant reference. By utilizing the interference of the wireless channel, the communication scheme designed in this paper can save communication resources, amount of computation, and energy proportionally to the number of spacecraft. The exact discrete-time model and approximate discrete-time model of the consensus-based spacecraft tracking system are given. Then the framework for the design of an event-triggered control scheme for the exact discrete-time system via its approximate models is developed, which avoids the periodic actuation, and Zeno behavior is proved to be excluded. Furthermore, the control scheme can handle the presence of the unknown fading channel. Finally, simulation results are presented to demonstrate the effectiveness of the control strategy. 相似文献
146.
《中国航空学报》2023,36(5):286-305
Commercial aircraft crews have experienced a trend from five-person crew to dual-pilot crew. Arised from both technological and market demands, Single Pilot Operations (SPO) is considered an important development direction in modern aviation technology. In this paper, starting from Dual-Pilot Operations (DPO), the piloting process, decision-making process and decision-making mode of DPO for commercial aircraft are studied to obtain the operational requirements of SPO. Then, based on above analysis, the operational mechanism of SPO is studied and the core technology of SPO mode is proposed. Next, a new closed frequent bicluster mining algorithm named FsCluster is proposed for the optimization of the SPO model, and the other efficient bicluster mining algorithm named TsCluster is proposed for the analysis and verification of the SPO model. Finally, a typical flight phase scenario is modelled by Magic System of System, and combined with the proposed algorithms for analysis and verification to determine whether the SPO mode can meet the DPO requirements. 相似文献
147.
针对通信网络拓扑结构切换下的协同制导问题,提出了一种预定时间协同制导方法(PTCGL),以保证拓扑切换下的预定时间分组收敛。首先,建立三维飞行器协同制导模型和拓扑切换下的分组协同架构:组间利用小组领队飞行器之间的协作实现分组配合,组内则通过有向通信实现组协同。随后,在通信网络拓扑结构切换的情况下,结合牵制控制和预定时间理论,基于M矩阵假设的牵制分组误差和预定时间尺度函数提出拓扑切换三维预定时间协同制导律。进一步,考虑拓扑切换驻留时间,利用Lyapunov理论证明在通信拓扑切换的情况下,该制导律可实现预定时间收敛。最后,数值仿真结果验证了所提出的协同制导方法可实现在拓扑切换下的预定时间收敛、保证分组协同打击。 相似文献