基于改进NSGA-II算法的风力机叶片多目标优化设计

一种结合了精英控制策略和动态拥挤距离方法的改进的快速支配排序算法(Fast and elitist non-dominat-ed sorting genetic algorithm,NSGA-Ⅱ)被用于风力机复杂的多目标优化设计中。作为此算法的应用算例,以风轮的年发电量最大、叶片的质量最小和叶片根部的极限推力最小为目标,分别进行了两目标和三目标的1.5 MW风力机叶片的优化设计。研究表明:两目标优化给出的Pareto最优解集分布在一条曲线上,而三目标的优化结果基本分布在一个有明显边界的五阶曲面上。同时也可以看出,此算法在处理风力机多目标优化问题取得了良好的效果,给出的是一个Pareto最优解集,而不是传统优化方法追求的单个最优解,为风力机多目标优化设计提供通用的算法。     

高校合同管理与法律风险预防研究——兼析我校近年来发生的系列合同纠纷案件

随着社会主义市场经济的发展,高校参与社会经济生活的范围越来越广。作为高校与社会经济生活中发挥着纽带和桥梁作用的合同管理也就凸现其重要性。做好合同管理,防范法律风险,成为高校在对外合作交流中的一项重要职责。本文拟结合近年来我校在对外经济往来方面发生的合同纠纷案例,探讨加强合同管理与预防法律风险的重要意义。     

促进空中乘务专业学生岗位职业能力培养的探索

根据行业需求,在明晰空中乘务专业人才培养目标的基础上,结合该专业主要就业岗位重点分析了空中乘务人员岗位知识能力要求,根据我院教学实践经验分别从“民航基础知识”、“旅客服务素养专项技能训练”两个层面,提出了促进空中乘务专业学生岗位职业能力培养的教学方法。     

基于XML的遥测数据管理

结合XML与关系数据库各自在数据管理上的优势,设计了基于XML的遥测数据管理系统。其中,对遥测数据的存储除了直接XML结构化存储外,还提出了“数据分段”的方法存储大数据量参数,在实际系统运行中表现出很高的数据检索效率。由于XML文档在Internet数据发布上具有先天的优势,系统可直接将未解析的XML文档输出到客户端,因此提高了遥测数据的发布能力。     

Improving the estimation of zenith dry tropospheric delays using regional surface meteorological data

Global Navigation Satellite Systems (GNSS) are emerging as possible tools for remote sensing high-resolution atmospheric water vapour that improves weather forecasting through numerical weather prediction models. Nowadays, the GNSS-derived tropospheric zenith total delay (ZTD), comprising zenith dry delay (ZDD) and zenith wet delay (ZWD), is achievable with sub-centimetre accuracy. However, if no representative near-site meteorological information is available, the quality of the ZDD derived from tropospheric models is degraded, leading to inaccurate estimation of the water vapour component ZWD as difference between ZTD and ZDD. On the basis of freely accessible regional surface meteorological data, this paper proposes a height-dependent linear correction model for a priori ZDD. By applying the ordinary least-squares estimation (OLSE), bootstrapping (BOOT), and leave-one-out cross-validation (CROS) methods, the model parameters are estimated and analysed with respect to outlier detection. The model validation is carried out using GNSS stations with near-site meteorological measurements. The results verify the efficiency of the proposed ZDD correction model, showing a significant reduction in the mean bias from several centimetres to about 5 mm. The OLSE method enables a fast computation, while the CROS procedure allows for outlier detection. All the three methods produce consistent results after outlier elimination, which improves the regression quality by about 20% and the model accuracy by up to 30%.     

基于Multi—Agent的空中交通流量仿真研究

针对传统空中交通流量仿真过程中灵活性和智能性的不足，将分布式人工智能Multi—Agent的理论和方法应用到空中交通流量管理领域中，提出了基于Muhi-Agent的空中交通流量仿真方法。介绍了空中流量管理的体系结构和流量管理的具体措施，详细设计了与流量仿真相关的重要Agent，包括航班Agent、航路Agent、机场终端区Agent和区域流量管理Agent等，探讨了各Agent的内部运行机制和在流量管理中的职能，构建了基于Multi．Agent的空中交通流量仿真子系统的整体框架．为实际空中交通流量管理系统的建设提供重要的指导和拳者。     

Supertyphoon Hagibis action in the ionosphere on 6–13 October 2019: Results from multi-frequency multiple path sounding at oblique incidence

The purpose of the present paper is to describe the observations of the variations in the parameters of HF radio waves propagating through the ionosphere when the action of the super typhoon Hagibis on 6–13 October 2019 occurred. The observations have been made with the Harbin Engineering University (the People's Republic of China) multi-frequency multiple path radio system involving the software-defined technology. The action of the super typhoon has been shown to be accompanied by enhanced atmospheric wave activity acting to generate wave processes with periods of 10 to 120 min. Coupling in the atmosphere–upper-atmosphere–ionosphere system has been confirmed to be carried out with atmospheric gravity waves. The ionosphere underwent the greatest impact on those days when the supertyphoon had maximum energy, on 8, 10, and especially 9 October 2019, and when it was found to be in an ～2,500–3,000-km distance range from the propagation path midpoints. Under the action of wave processes, the height of the reflection region was observed to oscillate within the ±(30–90 km) limits. The amplitude of the quasi-periodic variations in the ionospheric F-region electron density was estimated to be 10–12% for periods of ～20 min, and 30–60% for periods of ～60–120 min. The joint action of the dusk terminator and the supertyphoon has been confirmed to enhance wave activity in the ionosphere. Similar effects for the dawn terminator have not been detected.     

Evaluation of simulation-based training for aircraft carrier marshalling with learning cubic and Kirkpatrick’s models

Simulation-based training is a promising way to train a carrier flight deck crew because of the complex and dangerous working environment. Quantitative evaluation of simulation-based training quality is vital to make simulation-based training practical for aircraft carrier marshalling.This paper develops a personal computer-based aircraft carrier marshalling simulation system and a cave automatic virtual environment(CAVE)-based immersive environment. In order to compare the training effectiveness of simulation-based training and paper-based training, a learning cubic model is proposed and a contrast experiment is carried out as well. The experimental data is analyzed based on a simplified Kirkpatrick’s model. The results show that simulation-based training is better than paper-based training by 26.80% after three rounds of testing, which prove the effectiveness of simulation-based aircraft carrier marshalling training.     

浅谈冬季恶劣天气签派放行攻略

针对冬季机场容易出现的恶劣天气特点,主要从降雪跑道结冰、大雾低能见两个主要恶劣天气着手,分析飞行签派员放行攻略。     

Orbital rendezvous mission planning using mixed integer nonlinear programming

The rendezvous and docking mission is usually divided into several phases, and the mission planning is performed phase by phase. A new planning method using mixed integer nonlinear programming, which investigates single phase parameters and phase connecting parameters simultaneously, is proposed to improve the rendezvous mission’s overall performance. The design variables are composed of integers and continuous-valued numbers. The integer part consists of the parameters for station-keeping and sensor-switching, the number of maneuvers in each rendezvous phase and the number of repeating periods to start the rendezvous mission. The continuous part consists of the orbital transfer time and the station-keeping duration. The objective function is a combination of the propellant consumed, the sun angle which represents the power available, and the terminal precision of each rendezvous phase. The operational requirements for the spacecraft–ground communication, sun illumination and the sensor transition are considered. The simple genetic algorithm, which is a combination of the integer-coded and real-coded genetic algorithm, is chosen to obtain the optimal solution. A practical rendezvous mission planning problem is solved by the proposed method. The results show that the method proposed can solve the integral rendezvous mission planning problem effectively, and the solution obtained can satisfy the operational constraints and has a good overall performance.