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。     

现代战斗机最优过失速和高速转弯机动

通过分析水平面内的最快转弯和最小半径转弯，研究了现代战斗机的最优过失速机动和高速机动。利用最优控制理论，讨论和分析了最优倾侧角控制和推力控制规律。典型示例飞机的数值仿真计算结果表明，最优高速转弯轨迹是Ｂ、Ｃ和Ｓ等各段子弧的相应组合，它与发动机推力、飞行高度、端点马赫数、过载和空气动力约束等相关；提高发动机推力亦可减小最优转弯时间。     

轴类零件图计算机辅助绘制系统的开发

介绍在AutoCAD2004平台上,利用二次开发系统及其下拉菜单、VLISP语言等控制模块程序而开发轴类零件图绘制系统。软件采用下拉式菜单技术和屏幕图形可视化,使用户方便快捷地进行绘制各种轴类零件图,从而减轻设计人员在绘制轴类零件图的重复性工作,具有交互性好、使用方便及扩展性好等特点。     

某平尾旋转频率降低原因分析及改进

对某型飞机全机共振试验中出现的平尾旋转频率降低的问题进行了详细的分析，并对影响平尾旋转频率降低的部位进行了测试，找出了原因，进行了排除。     

智商、情商与高职高专英语教学——高职高专英语应用能力考试教学方法改革探析

通过对情商及其基本内涵的分析，指出智商是定的，但语言教育工作者可以通过后天的培养，提高学生的情商，最终使情商与写长法、英语学得与习得结合起来服务于英语教学。     

高职院校学分制实施过程中存在的问题与对策

分析部分高职学院在实行学分制管理过程中遇到的外部和内部的问题,提出解决对策。     

高校收费的定价模型与助学贷款有关问题的研究

本文论述了高校收费定价应充分考虑居民收入水平等诸多方面,国家应成为办学的主体。要解决贫困生上大学的学费及生活费问题,就必须抓紧建立全国性个人征信机构,成立国家助学贷款政策性银行。     

Solar neutron events as a tool to study particle acceleration at the Sun

The Sun provides unique opportunities to study particle acceleration mechanisms using data from detectors placed on the Earth’s surface and on board spacecrafts. Particles may gain high energies by several physical mechanisms. Differentiating between these possibilities is a fundamental problem of cosmic ray physics. Energetic neutrons provide us with information that keeps the signatures of the acceleration site. A summary of some representative solar neutron events observed on the Earth’s surface, including associated X and γ-ray observations from spacecrafts is presented. We discuss evidence of acceleration of particles by the Sun to energies up to several tens of GeV. In addition, a recent solar neutron event that occurred on September 7th 2005 and detected by several observatories at Earth is analyzed in detail.