基于利益相关者保护视角的互联网金融监管研究

互联网金融的发展还处于起步阶段,现有文献更多地从互联网金融发展全局角度来研究其监管问题。鉴于互联网金融发展初期的不规范与脆弱性,认为互联网金融不仅仅需要监管,更要保护。基于利益相关者保护的新视角,从狭义互联网金融的三种模式,即P2P网贷、大数据金融以及众筹融资三种模式出发,分析三种模式的利益相关者及其风险传导模式,提出了互联网金融如何保护与监管并进的政策建议。     

非营利组织的管理：香港的启示

由于政府失灵和市场失灵的存在，社会的良好运行不仅需要政府和企业，还需要大量第三部门的存在。长期以来，我国的非营利组织是由国家出资成立并负责日常管理的，但是这并不符合现代政府职能的发展要求，在改革过程中由政府管理的非营利组织不仅成为政府的负担，同时也与其自身发展需要不符。因此政府如何将原先由其管理的非营利组织交给社会并促其健康成长是非常重要的。中国香港由法定程序所设立机构的日常运行模式是目前可资借鉴的改革方向之一。     

外语学习真实性语境的课堂实现

在无外语本族语者参与或无真实交际需要的大学英语课堂上,探讨如何利用英语影片的教学来实现外语学习的真实性语境,二语习得和外语教学研究表明,外语学习亟需与真实的语境相结合,才能规避母语语境补缺带来的负迁移。     

航空运输业排放权交易研究

首先介绍了排放权交易的起源、概念、经济理论和国际法基础,然后重点总结了欧盟将航空运输活动纳入排放权交易的主要内容,最后,提出了我国民航实施排放权交易需解决的关键问题。     

高校基层党支部组织生活创新的基本路径

当下高校基层党支部组织生活存在的诸多问题,可以通过创新机制加以解决.创新必须坚持解放思想、实事求是、与时俱进、求真务实的原则,从根本上保证创新的正确方向,并通过创新思路观念、规章体制、内容形式、评价机制四条路径加以进行.     

基于模糊理论的直升机驾驶舱人机工效综合评价研究

影响驾驶舱人机工效的因素非常多，交联关系复杂，在对其进行综合评价时，必须考虑系统因素内在的模糊性、评价指标与原则定义上的模糊性以及评价专家认识上的模糊性。探讨应用模糊综合评价的方法进行驾驶舱人机工效评价，给出了应用模糊综合评价法进行人机工效评价的一般过程和处理方式，并用典型事例进行验证。     

无人机机载导弹落角和时间控制导引律研究

改进了一种能同时控制命中角和命中时间的修正比例导引律,将其用到无人机机载空对地导弹中,将其中的剩余时间估计加入了命中角约束的影响,旨在保证无人机机载导弹垂直命中目标的同时,使命中时间更为准确.通过对此导引律和一种仅考虑垂直命中角约束的修正比例导引律以及和改进前导引律的比较,仿真表明,此导引律使无人机机载导弹能在保证垂直...     

Station-keeping control for a stratospheric airship platform via fuzzy adaptive backstepping approach

This paper presents a novel approach for station-keeping control of a stratospheric airship platform in the presence of parametric uncertainty and external disturbance. First, conceptual design of the stratospheric airship platform is introduced, including the target mission, configuration, energy sources, propeller and payload. Second, the dynamics model of the airship platform is presented, and the mathematical model of its horizontal motion is derived. Third, a fuzzy adaptive backstepping control approach is proposed to develop the station-keeping control system for the simplified horizontal motion. The backstepping controller is designed assuming that the airship model is accurately known, and a fuzzy adaptive algorithm is used to approximate the uncertainty of the airship model. The stability of the closed-loop control system is proven via the Lyapunov theorem. Finally, simulation results illustrate the effectiveness and robustness of the proposed control approach.     

Optimal guidance based on receding horizon control for low-thrust transfer to libration point orbits

This paper addresses the design and computation of a guidance law for a transfer mission from an orbit near the Earth to a halo orbit around the libration point L₂ in the Sun–Earth system. The guidance law, which is designed based on receding horizon control and compensates for launch velocity errors that are introduced by inaccuracies of the launch vehicle, is solved using the generating function method. During the design of the closed-loop guidance law, the entire transfer mission, which is considered a nonlinear optimal control problem, is evaluated to obtain a nominal reference trajectory. Using the launch velocity errors and the uncertainty of the model, a spacecraft controlled by the proposed guidance law tracks the reference trajectory. Furthermore, the original Riccati differential equation in the receding horizon control algorithm is replaced by an equivalent convenient form of the Riccati differential equation that is based on the generating function. The high-efficiency solution of the equivalent equation avoids the online direct integration of the original Riccati differential equation, which significantly increases the computational efficiency for the receding horizon control problem. Numerical simulations using a nonlinear bicircular four-body model demonstrate the capabilities of the proposed receding horizon guidance law for the transfer mission. In addition, the generating function method improves the computational efficiency by at least one order of magnitude over the backward sweep method in solving the receding horizon control problem.     

油气式缓冲器充填参数试验过程动态模拟方法

提出一种新的关于油气式缓冲器充填参数试验过程的动态模拟方法。该方法是按照一定的设计及计算程序，以自动的方式替代传统的人工操作，不但效率高，而且效果好，更新了传统的“试凑”概念，开拓了一条设计新途径。