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综述了为验证增强战斗机机动性(EFM)计划、衡量过失速机动飞行的可行性及其在近距空战中的战术价值,X-31A飞机在气动布局、大迎角抗偏离设施、推力矢量系统以及飞控系统方面的特点;介绍了X-31A飞机的有关飞行试验情况,特别是循序渐近的四种过失速机动动作以及空战效能评估结果。结果表明,X-31A飞机气动布局合理,能完成过失速机动飞行。且过失速机动技术和推力矢量组合,可以大大地提高飞机近距空战的作战效能。 相似文献
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Satellite communications technology has reached the stage at which it is feasible to develop a reliable military tactical communications system using small transportable Earth terminals. This paper discusses the design considerations involved for a multiple-access system, with particular reference to the Earth terminals. 相似文献
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战术弹飞行力学软件系统设计 总被引:4,自引:0,他引:4
从战术弹飞行力学软件系统的设计开发角度,提出了软件系统的设计指导思想,对软件系统基本运行流程进行了分析研究,完成导弹设计不同阶段有关飞行力学问题研究的应用软件设计开发。编制了系统的符号词典和软件文档。在软件系统设计时考虑多种语言程序之间的接口设计及运行环境,并就软件系统进一步开发研究进行了探讨。完成了战术弹飞行力学软件系统的设计。 相似文献
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A family of 4-wire electronic equipments is being developed for use in a tactical switching system for the field army. The characteristics and design of two automatic switchboards to be used in the system are discussed, as well as the signaling methods and numbering plan that are employed. 相似文献
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A digital autopilot design was developed for a small laser-guidedtactical missile. The multiloop design was developed in the w plane and analyzed by time domain simulation. Performance is as good or better than the current analog version, thus demonstrationg the feasibility of digital guidance technology in tactical missile applications. 相似文献
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Development of the μSCIRASTM (pronounced micro-Cyrus) multisensor for a period of over six years has produced a practical MEMS Inertial Measurement Unit (IMU). Using only three silicon sensors, a full-up IMU suitable for tactical grade navigation and guidance applications has been achieved. Iterative improvements in silicon sensor design and bulk micromachining processes have matured to the point where an IMU with an attractive price/performance ratio is now producible. This paper summarizes the design features and test results for an IMU with <100 deg/hr performance. Test results are shown for rate bias and acceleration bias over temperature. Production of this initial member of the μSCIRAS product family begins this year to support applications including guided artillery shells, technology insertion to decrease missile costs, navigation of remotely-piloted vehicles, dismounted soldier location devices and other navigation aids. The small size of this silicon multisensor and its ability to measure both angular rotation rate and linear acceleration provides a useful advantage in product packaging, cost, size, and system testing. The μSCIRAS Inertial Sensor Assembly (ISA) is housed in a 2 cubic inch package weighing less than 5 ounces (140 grams) requires less than 0.8 Watts of power. Continuing development will lead to greatly improved performance on the order of 1 deg/hr at low prices in high-volume production 相似文献
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《中国航空学报》2020,33(1):255-270
This study creates and combines the general maneuver libraries for fixed-wing aircraft to implement tactical maneuvers. First, the generalized maneuver libraries are established by analyzing the characteristics of tactical maneuvers required in battlefields. The 7th order polynomial is applied to both the creation of the maneuver libraries and the generation of the trajectories or flight paths for modal inputs. To track the desired trajectory, we design the Attitude Command Attitude Hold (ACAH) system and the Rate Command Rate Hold (RCRH) system using Model Following Controller (MFC). Moreover, the Line-of-Sight (LOS) guidance law is designed. In particular, the CONDUIT® is employed to optimize the gains so that the control systems meet the aircraft Handling Qualities (HQ) criteria. Finally, flight simulations are performed for the longitudinal loop, immelmann-turn, and climb-slalom-descent maneuvers to verify that tactical aggressive maneuvers are realizable via the combination of maneuver libraries. This study can contribute to the development of flight techniques for aircraft tactical maneuvers and to the revision of air force operational manuals. 相似文献
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按照飞行器设计的基本原理并结合无人机特点,对侦察、监视类战术无人机总体参数与性能参数进行了相关性分析,找出了两者可能存在的数学关系,得到10个经验公式和一些重要参数的取值范围,可为战术无人机的概念设计提供有用的数据和参考。 相似文献
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On February 8, 1969, an experimental tactical communications satellite, TACSAT I, was successfully placed in synchronous orbit at the equator off the coast of South America. This paper concerns itself with a family of SHF tactical satellite communications ground terminals utilizing the SHF capability of that satellite. The material presented provides the system concepts necessary for the understanding of the ground terminals, their relationship to the satellite, and some insight into the design problems encountered during the development of a family of five types of terminals. The system concepts are presented in terms of communication modes, frequency assignments, and implementation of the respective modes. The beacon system for frequency control and signal acquisiticn siticn is described along with the factors involved in design of equipment implementing the analog FM, the alert message, frequency hopping, and, differential phase-shift keyed (DPSK) modes. The final configurations of each of the five terminals are described and illustrated through photographs and generalized block diagrams, and the capability of each is briefly outlined. 相似文献
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仿真技术的应用范围已从作战领域扩展到武器型号研制领域。阐述仿真、仿真模型和仿真系统的基本概念和特点,以及分布交互仿真和虚拟仿真与型号研制的关系。以战术导弹为例探讨了仿真系统在型号研制、试验、评估和降低成本中的重要作用。 相似文献
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为满足作战需要 ,改善导弹的总体性能 ,又有利于降低研制成本 ,对图像制导导弹的导引头最大跟踪角速度、极限框架角、搜索方案以及导弹的速度方案 ,进行了分析设计。以此为例 ,对飞行力学在导弹总体与分系统设计中的应用进行了说明。研究结果表明 :飞行力学是协调导弹总体与各分系统之间关系的重要手段 ,在导弹总体和各分系统的设计过程中 ,积极主动地应用飞行力学进行综合设计 ,可获得最佳的总体性能。 相似文献
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MILDATA was an Army-sponsored exploratory development study in the area of digital computer technology. Its objective was to explore and evaluate new organizational concepts for hardware and software in a tactical command control information system (CCIS) and to develop new measures of effectiveness and methods for evaluating system performance. It was assumed that the MILDATA system would be operational in the field army during the time frame 1975-1985. A unique feature of the MILDATA concept is an unprecedented degree of modularity which provides flexibility to fulfill a wide variety of tactical data processing requirements. This paper supplies necessary background on CCIS requirements and develops modular design criteria. It then summarizes MILDATA study requirements and the general nature of the results obtained and outlines a program of future work. Finally, an attempt is made to systematize the experience gained during MILDATA as an aid to the organization of future exploratory development studies. 相似文献
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The allure of the solid state optical gyros is being challenged by the invention of a new spinning mass device, providing superior low noise drift performance, high reliability at a very low cost. The Minitact is a unique two axis gyroscope advancing the technology of spinning mass devices to set new low cost standards. Minitact provides all the low noise performance benefits of tuned rotor gyroscopes without the vagaries of fixture suspension systems. The Minitact design integrates together the advantages of a spherical hydrodynamic gas bearing and a three axis permanent magnet DC commutated, motor and torquer, into miniature two aids gyroscope with a dynamic range of greater than 10-7. The design is described and performance data presented illustrating the capability of this low cost next generation rate gyroscope. The Minitact is the result of Integrated Product Development (IPD) and Design to Unit Production Cost (DTUPC) design processes and is expected to become the tactical performance benchmark 相似文献
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Best P.S. Collins D.J. Piccione D. Ferrett D. 《Aerospace and Electronic Systems Magazine, IEEE》1999,14(4):5-8
The PM N-V/RSTA is procuring the Driver's Vision Enhancer (DVE) thermal imaging system for use in combat and tactical wheeled vehicles. The DVE uses uncooled forward looking infrared technology compared to the I2 technology currently in the field. During the development of the DVE several issues were raised regarding how specific aspects of system design were related to driver performance. As a result, DCS Corporation developed a data collection effort to provide the DVE project leader with needed performance data that could act as a foundation for making program decisions 相似文献
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Podlesak T.F. Carter J.L. McMurray J.A. 《Aerospace and Electronic Systems Magazine, IEEE》1990,5(12):25-28
A high-voltage opening switch that uses gate-turnoff thyristors (GTOs) in series and successfully operates at voltages higher than the rated voltage of the individual devices has been demonstrated. The switch design and construction are described, and experimental results are given. The demonstration system is rated at 5 kV and uses 1-kV devices. A larger 24-kV system is under design and will use 4.5-kV devices. In order to design the 24-kV switch, the safe operating area of the large devices must be thoroughly known 相似文献