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GPS Satellite Advancements and its Future GPS卫星的发展及其未来
Pub Date : 2020-05-12 DOI: 10.24321/2456.1398.202001
Gopal Kochhar
This paper gives an brief introduction of global positioning system, its generations, the future and progressions that are attained by the GPS and tracking systems. The latest usage and the comparative study ofthe GPS satellites that are launched and are operational till date. How to cite this article: Kochhar G, Agarwal A, Athaiya A et al.GPS Satellite Advancements and its Future. J Adv Res Instru Control Engi 2020; 7(1): 1-4. DOI: https://doi.org/2010.24321/2456.1398.202001
本文简要介绍了全球定位系统,以及GPS和跟踪系统的产生、未来和发展。目前已发射和运行的GPS卫星的最新使用情况和比较研究。本文来源:Kochhar G, Agarwal A, Athaiya A等。gps卫星的发展与未来。工程学报(自然科学版);7(1): 1 - 4。DOI: https://doi.org/2010.24321/2456.1398.202001
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引用次数: 0
LED Heatsink Optimization using Self Powered Active Cooling 使用自供电主动冷却的LED散热器优化
Pub Date : 2018-04-03 DOI: 10.24321/2456.1398.201801
Deepa Chandran
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引用次数: 0
Concept of Operations to System Design and Development-An integrated system for Aircraft Mission Feasibility Analysis using STK Engine MATLAB and LabVIEW 系统设计与开发的操作概念——基于STK发动机、MATLAB和LabVIEW的飞机任务可行性分析集成系统
Pub Date : 2016-02-27 DOI: 10.5121/ijics.2015.5401
Princy Randhawa, Vijay Shanthagiri, Vibhu Johar, Kanika Sharma
In recent times, there has been a significant rise in usage of aircrafts in surveillance and reconnaissance missions. Not all the aircrafts survive the harsh testing conditions put forth by the enemy regions. Aircraft Survivability Analysis gives the measure of the chances of survival for different counter strategies. The mission would be recalculated if particular sortie does not fall within the physical boundary of the performance of an aircraft. This is required both for the success of the mission and the survivability of the aircraft in the harsh enemy conditions. A system is envisioned comprising of the accurate modeling of the physical world and the accurate model of control system. An interoperable system which can work seamlessly together will provide mission planners, System integrators, aeronautical/ aerospace engineers a milieu wherein the Control System designer who is found wanted as far as the physical world is concerned is given a system which can simulate the real world in lab conditions. To achieve this, we combine the two most promising environments prevalent in the industry today namely Systems tool kit for modeling the operational environment MATLAB and LabVIEW for modeling the control system environment. Using a Math script window of LabVIEW, we have designed the aircraft model and controlling the variables of an aircraft using a simulation loop of a LabVIEW. The different flight conditions were arrived using Orthogonal Array (OA) based on different Aircraft weight, Altitude, Mach number configurations. This attempts to span the aircrafts across the regimes in aircrafts flight envelope. A system comprising of both, with seamless UDP based connection between the two is developed to expedite the process of development of feasible control system design and verification which allows the aircrafts to undertake complex mission. This system we believe would answer questions of limits of the aircrafts maneuverability and survivability in terms of its limitation concerning control system design and development of commercial fighter aircrafts, UAV's and Quad copters.
最近,在监视和侦察任务中使用飞机的次数大大增加。并非所有的飞机都能经受住敌区严酷的考验。飞机生存能力分析给出了不同对抗策略的生存机会。如果特定架次不属于飞机性能的物理界限,则将重新计算任务。这对于任务的成功和飞机在恶劣敌人条件下的生存能力都是必需的。设想了一个由物理世界的精确建模和控制系统的精确模型组成的系统。一个可以无缝协同工作的可互操作系统将为任务规划者、系统集成商、航空/航天工程师提供一个环境,在这个环境中,被发现需要的控制系统设计师可以在实验室条件下模拟真实世界。为了实现这一目标,我们结合了当今行业中最具前景的两个环境,即用于建模操作环境的系统工具包MATLAB和用于建模控制系统环境的LabVIEW。利用LabVIEW的数学脚本窗口设计了飞机模型,并利用LabVIEW的仿真循环控制了飞机的变量。基于不同的飞机重量、高度、马赫数配置,采用正交阵列法(OA)得到了不同的飞行条件。这试图跨越飞机在飞机的飞行包线制度的飞机。一个由两者组成的系统,在两者之间开发了基于UDP的无缝连接,以加快可行控制系统设计和验证的开发过程,使飞机能够承担复杂的任务。我们认为该系统将回答飞机机动性和生存能力的限制问题,因为它的限制涉及商用战斗机、无人机和四轴直升机的控制系统设计和发展。
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引用次数: 6
Design and Analysis of Fuzzy Logic, Sliding Mode, Dynamic Sliding Mode and PID Controllers for Level Control in A Prototyped Split Range Plant 模糊控制器、滑模控制器、动态滑模控制器和PID控制器的设计与分析
Pub Date : 2015-10-15 DOI: 10.26634/JIC.3.4.3723
S. Harivardhagini, A. Raghuram
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引用次数: 1
Position Control of PMLSM with Space Vector Pulse Width Modulation Using Matlab 空间矢量脉宽调制永磁同步电机的位置控制
Pub Date : 2015-10-15 DOI: 10.26634/JIC.3.4.3721
K. Shankar, B. Arundhati
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引用次数: 0
A Study of Gauge Repeatability and Reproducibility Characteristics on Critical Parameters of A Cylinder Liner 某缸套关键参数的量规重复性及再现性特性研究
Pub Date : 2015-10-15 DOI: 10.26634/JIC.3.4.3724
K. P. Babu, A. Priyanka, K. Kavyasri
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引用次数: 2
Design of Fuzzy Controller Using Single Linear Nominal Plant for Mass-Spring-Damper System 质量-弹簧-阻尼系统的单线性标称模糊控制器设计
Pub Date : 2015-10-15 DOI: 10.26634/jic.3.4.3722
R. Tanna, A. K. Deb
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引用次数: 0
Fuzzy Back-Propagation Network Based Controller for Power Quality Improvement Using UPQC 基于模糊反向传播网络的UPQC电能质量改进控制器
Pub Date : 2015-10-15 DOI: 10.26634/jic.3.4.3720
V. V. N. Reddy, D. V. A. Kumar, K. V. Reddy
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引用次数: 0
Trichotomous Exploratory Data Analysis [TriEDA]: A Post Hoc Visual Statistical Cumulative Data Analysis Instrument Designed to Present the Outcomes of Trichotomous Investigative Models 三分形探索性数据分析[TriEDA]:一种旨在呈现三分形调查模型结果的即时可视化统计累积数据分析工具
Pub Date : 2015-07-15 DOI: 10.26634/JIC.3.3.3578
J. E. Osler
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引用次数: 0
Design of PID Controllers for Unstable Second Order Plus Time Delay Systems by Equating Coefficient Method 二阶加时滞不稳定系统的PID控制器设计
Pub Date : 2015-07-15 DOI: 10.26634/jic.3.3.3579
C. R. Kishore, R. P. Sree
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引用次数: 0
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