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A Multi-Objective Design Optimization Procedure for a General Control System

机译:通用控制系统的多目标设计优化程序

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With the advancement in new materials and techniques, smooth and high performance operation of critical systems, such as flight simulators, satellite navigators and robot arms, are expected. To give examples, a long duration for space shuttle after its take off cannot be tolerated in terms of its system dynamics and stability as well as high off-the-target position errors for a pick-and-place robot. In most of these military and industrial systems, control objectives are more than one and mostly intensified at minimizing overshoot from steady state response with a minimum system settling time. Stability of the systems is also another objective. Any such system can be idealized as a combination of mass-spring-dashpot system and its stability conditions can be determined from the locations of the poles of the system characteristics equation. As it is well known, when the damping ratio is zero or negative, the poles are located at the right-hand side of the s-plane presenting instability. In this study, a general mass-spring-dashpot system is considered first. Then, its mathematical differential equation is transformed into Laplace domain to formulate undamped natural frequency and damping ratio. By choosing these two as system design variables, numerical constraints are impinged on system settling time, percent overshoot and time to reach to maximum peak. Multi-objective optimization is performed using powerful method of Global Criterion Method. The cost functions are minimization of system settling time, the percent overshoot and time to reach maximum peak. Design specifications are suggested for this particular configuration in terms of relations between mass, spring and dashpot. It is intended to lay out a design optimization procedure to system designers in choosing mass, spring and dashpot characteristics for a stable system operating optimally under prescribed constraints. It is also shown that the Global Criterion Method is a versatile optimization tool for multi-criterion problems.
机译:随着新材料和新技术的发展,人们期望关键系统(例如飞行模拟器,卫星导航仪和机器人手臂)能够平稳高效地运行。举个例子,就其系统动力学和稳定性以及取放机器人的高偏离目标位置的误差而言,航天飞机起飞后的持续时间不能容忍。在大多数这些军事和工业系统中,控制目标是不止一个,并且在以最小的系统建立时间将稳态响应的过冲最小化的情况下,其控制目标得到了最大程度的增强。系统的稳定性也是另一个目标。任何这样的系统都可以理想化为质量-弹簧-阻尼系统的组合,并且其稳定性条件可以从系统特性方程的极点位置确定。众所周知,当阻尼比为零或负时,磁极位于s平面的右手侧,表现出不稳定性。在这项研究中,首先考虑一般的质量弹簧-阻尼系统。然后,将其数学微分方程转换为拉普拉斯域,以制定无阻尼的固有频率和阻尼比。通过选择这两个作为系统设计变量,数值约束会影响系统稳定时间,超调百分比和达到最大峰值的时间。使用强大的全局准则方法执行多目标优化。成本函数是最小化系统建立时间,超调百分比和达到最大峰值的时间。根据质量,弹簧和减震器之间的关系,建议针对此特定配置的设计规格。它旨在为系统设计人员设计一种优化设计程序,以选择质量,弹簧和阻尼特性,以使稳定的系统在规定的约束条件下以最佳方式运行。还表明,全局准则方法是针对多准则问题的通用优化工具。

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