基于遗传算法的平流层飞艇路径规划设计

利用传统线性化方法--小扰动法将模型线性化,结合平流层飞艇的工作特性,把飞艇上升运动看成是纵向基准运动和横侧向扰动运动.然后采用最小值原理,根据飞艇的控制量和边界条件,设计和优化飞艇的上升轨迹,其性能目标函数是从初始点到目标点运动过程中能量消耗最小.利用遗传算法,在运动模型和控制量变化的共同约束作用下,求取目标函数的最小值.最后根据飞艇实际工作过程,对仿真结果分析表明,该方法具有实际应用价值.     

平流层通信平台MAC层的调度方案建模及仿真

平流层升空平台能够满足可提供战时服务、能快速部署,适用于区域性覆盖.为满足平台支持的多用户、多优先权、综合业务的接入策略并解决资源动态分配问题.提出了一种可以满足平台MAC层的服务质量(QoS)和动态带宽分配的调度架构,架构包括移动中心站(MCS)对移动站(MS)的带宽分配和移动站内上行业务的二级带宽调度架构,并根据不同业务需求采用不同的调度算法.仿真结果表明:调度方案能很好的满足所有类型业务的服务质量需求.并提供了较好的公平性,保证了架构的可行性.     

平流层飞艇热性能分析软件开发

为减少平流层飞艇的设计周期和设计试验经费,清晰准确地反映出平流层飞艇空间轨迹和温度场分布以及各种不同因素对轨迹和温度场分布的影响,自主开发了平流层飞艇热性能分析软件.通过建立平流层飞艇运动和热特性模型,利用VC++编程环境,对平流层飞艇在不同输入状态下的上升、浮空、下降过程中的轨迹和温度进行数值仿真,并利用图形显示界面进行显示.软件设计包括参数输入、中间计算和性能分析三个部分.软件将输出结果存储到ACCESS数据库中,增强了数据的可读性和交互性.从软件的运行结果反映出该软件涵盖面广、数据可靠、操作方便、界面生动等特点,达到预期设计目标.     

Mechanical property characterization of film-fabric laminate for stratospheric airship envelope

A stratospheric airship can offer a cost effective alternative to earth orbit satellites for telecommunication and science observation. To float in the stratosphere with very thin air density, the airship needs to be designed with envelope materials that are extremely light, flexible and of high strength. Film-fabric laminates, which consist of single plain woven fabric layer impregnated in polymer matrix and are laminated with thin films for environmental and leakage protection, have unique material characteristics compared to conventional composite structures that can be exploited in the design of the high altitude airship envelope materials. In this study, the material characterization of a film-fabric laminate developed for stratospheric airship envelop was conducted. First, uni-axial tests were performed for fabricated specimens to obtain tensile properties. The tests were done in the thermal chamber at low, room, and high temperatures to investigate the temperature dependency. Next, the effective tensile properties were predicted by geometrically nonlinear finite element analyses. The analyses were done for unit cells where the detailed fiber tow architecture was modeled discretely. The analysis results were compared to the test results and investigated focusing on the geometrical nonlinearity and the micro-structural behavior of the laminates.     

平流层演示验证飞艇实时仿真平台设计

在平流层飞艇的设计和研究中,飞行仿真可以有效验汪飞艇的动力学模型、控制器设计,检验飞艇的操纵性、飞行稳定性。同时,实时仿真技术可以提高飞艇性能,缩短研制周期。为解决上述问题,提出通过搭建飞艇的实时仿真平台,实现飞行仿真和实时仿真技术的统一。针对上海交通大学"致远一号"平流层演示验证飞艇,使用xPC target搭建了飞艇的实时仿真平台,完成了利用Simulink软件的动力学建模和控制系统设计,同时利用Flightgear飞行模拟器为仿真系统设计开发了视景仿真系统。进行仿真的结果显示,系统较好的实现了飞艇从上升到返回全过程飞行任务,视景系统直观准确地显示了飞艇在仿真过程中的状态变化,并可以为后续研究工作提供了依据。     

未来的大容量无线通信

未来通信的特征是传送各种业务信息的有、无线介质的数字混合体。在将来，面向个人的大容量卫星的平流层平台这两种空基平台会大有作为。文章介绍了这两种通信方式的最新进展。叙述了无线通信实现大容量的主要途径。结论：在大容量通信系统的发展过程中，空基平台无线通信将充满机会。     

Stratospheric balloons as a testbed for optical space communications technology

An experimental optical communications link between two stratospheric balloons is proposed as an intermediate step from limited ground laboratory tests to costly space operations. Such an experiment can overcome many environmental constraints encountered on the ground, and allows all measurements to be made directly in the antenna far field. Early performance demonstrations are possible which allow experimental trade-offs between alternative technologies and the verification of concepts, critical system parameters and subfunctions under near space conditions.     

Finite-time path following control for a stratospheric airship with input saturation and error constraint

This paper addresses the finite-time path following control problem for an under-actuated stratospheric airship with input saturation, error constraint, and external disturbances. To handle the adverse effect of input saturation, anti-windup compensators are employed and finite-time convergence of the saturated control solution is established. Error constraints of airship position and attitude are handled by incorporating a tan-type barrier Lyapunov function (TBLF) in guidance and attitude control schemes. Backstepping design is presented with the anti-windup compensators, the TBLF, and nonlinear disturbance observers which estimate the external disturbances. Stability analysis shows that the tracking errors of the airship position converge into a small set around zero within finite-time, the constrained requirements on the airship position and attitude are not violated during operation, and all closed-loop signals are guaranteed to be uniformly ultimately bounded. Compared with the conventional control scheme, simulation results illustrate that the proposed finite-time controller offers a faster convergence rate and a higher path following accuracy for the stratospheric airship.     

平流层通信在军事中的应用及相关技术

介绍了平流层通信的概念及其在军事中应用的特点。提出了实现平流层通信的关键技术,分析了通信平台的高度选择、载体选择以及平台动力和能源的解决办法。最后提出了平流层通信在军事中的几个应用。     

平流层飞艇试验场测试方法分析

针对平流层飞艇试验场测试需求,在分析飞艇关键系统构成的基础上,给出了试验场主要测试内容与方法,建立了试验场测试条件矩阵,给出了试验场测试项目总体流程;建立试验场测试模式,开展试验场测试系统与飞艇系统间接口设计,可为测试系统建设与试验场测试实施提供技术依据。