Zenith Pass Problem of Inter-satellite Linkage Antenna Based on Program Guidance Method

While adopting an elevation-over-azimuth architecture by an inter-satellite linkage antenna of a user satellite, a zenith pass problem always occurs when the antenna is tracing the tracking and data relay satellite （TDRS）. This paper deals with this problem by way of, firstly, introducing movement laws of the inter-satellite linkage to predict the movement of the user satellite antenna followed by analyzing the potential pass moment and the actual one of the zenith pass in detail. A number of specific orbit altitudes for the user satellite that can remove the blindness zone are obtained. Finally, on the base of the predicted results from the movement laws of the inter-satellite linkage, the zenith pass tracing strategies for the user satellite antenna are designed under the program guidance using a trajectory preprocessor. Simulations have confirmed the reasonability and feasibility of the strategies in dealing with the zenith pass problem.     

跳跃式跨大气层飞行弹道仿真分析

针对跳跃式跨大气层飞行弹道的特殊性,建立了其飞行动力学模型,在此基础上,对其弹道进行了仿真分析,得知乘波构型是跳跃式跨大气层飞行器理想气动布局,研究对比了跳跃弹道和惯性弹道的不同性能,结果表明跳跃飞行具有惯性飞行所无法比拟的突防能力。所得结论对跳跃式跨大气层飞行和未来新型武器装备的发展方向的研究具有一定的参考价值。     

电规准复合强化对强化层粗糙度的影响

本文采用电规准复合的方法对基体材料进行强化，结果表明强化层表面粗糙度有明显改善，且强化层的厚度主要取决于复合脉冲中的高能量脉冲。     

面向图形对象技术在风洞应变天平CAD系统中的应用

ARX是新一代面向对象的AutoCAD开发环境，在介绍其特征和功能的基础上，对风洞应变天平CAD系统开发中的一些关键技术进行了讨论，介绍了系统的总体结构，数据库的建立、阻力优化设计的数学模型和应用MFC实现图形用户化界面的设计思想与实现技术。ARX支持面向对象技术的特性改变了传统CAD软件的开发模,显示了广阔的应用前景。     

大电流矩形镉镍蓄电池组的FMEA分析

对大电流矩形镉镍电池进行了详细的失效模式与影响分析（ＦＭＥＡ），提出了相应的预防措施，对一南类电池的可靠性和维修性设计具有一定的帮助。     

高速公路融合式联网收费系统设计与实现

随着高速公路的迅猛发展以及计算机网络、通信等高新技术的发展 ,高速公路逐步走向智能化 ,并将最终发展成为智能交通系统 ( ITS Intelligent Transport System)。相应地 ,高速公路的收费技术呈现出网络化和智能化的趋势。文中介绍一种新型的融合式的自动收费系统 ,它采用智能卡技术 ,融合了人工收费方式和半自动收费方式 ,不仅支持现有系统的收费方式 ,而且还为将来采用电子收费 ( ETC Electronic Toll Collection)技术提供了接口功能 ,使系统具有较强的适应性和较好的扩展性 ,满足高速公路建设的要求     

运载火箭挡火帽可靠性增长研究

对运载火箭挡火帽可靠性进行了深入的分析，评估，对挡火帽材料的失效机理作了较为深入的探讨，在此基础上进行了可靠性试验及可靠性仿真计算，提出了挡火帽可靠生增长的措施。     

Fault-tolerant control with mixed aerodynamic surfaces and RCS jets for hypersonic reentry vehicles

This paper proposes a fault-tolerant strategy for hypersonic reentry vehicles with mixed aerodynamic surfaces and reaction control systems (RCS) under external disturbances and subject to actuator faults. Aerodynamic surfaces are treated as the primary actuator in normal situations, and they are driven by a continuous quadratic programming (QP) allocator to generate torque com-manded by a nonlinear adaptive feedback control law. When aerodynamic surfaces encounter faults, they may not be able to provide sufficient torque as commanded, and RCS jets are activated to augment the aerodynamic surfaces to compensate for insufficient torque. Partial loss of effective-ness and stuck faults are considered in this paper, and observers are designed to detect and identify the faults. Based on the fault identification results, an RCS control allocator using integer linear programming (ILP) techniques is designed to determine the optimal combination of activated RCS jets. By treating the RCS control allocator as a quantization element, closed-loop stability with both continuous and quantized inputs is analyzed. Simulation results verify the effectiveness of the proposed method.     

复合材料机翼油箱盖板的制造和质量控制

介绍了采用开模膨胀橡胶法制造带加强筋的复合材料机翼整体油箱油箱盖板的一次共固化的工艺方法.针对初期制造的油箱盖板存在的比较严重的质量问题,包括翘曲、筋条尺寸超差、大面积分层及空隙密集等,提出了相应的设计修改、工艺改进和质量控制措施,最终制造出合格的制件.通过了功能试验和飞行考核.     

新一代航空发动机转子叶尖高速磨复合加工技术

面对航空工业的快速发展,新一代航空发动机转子装配结构已完全有别于一、二代发动机,对转子叶片叶尖磨削也提出了更高的要求.近年来,随着三代发动机批量生产,其整体制造技术水平得到了较大的提升,但与国际先进航空发动机制造企业相比,个别制造工艺仍存在较大差距,高速叶尖磨工艺就是其中一例.