Performance Comparison of H-infinity and LQR Controllersfor the Pressure Regulation of a Hypersonic Wind Tunnel

Journal Title: International Journal of Modern Engineering Research (IJMER) - Year 2013, Vol 3, Issue 3

Abstract

Hypersonic wind tunnels are used to study the effect of air moving past the fighter planes, space vehicles and similar specimens under test. This paper aims to compare the performance of a h-infinity controller with that of a linear quadratic regulator (LQR) controller for regulating the pressure inside the settling chamber of a hypersonic wind tunnel. The linear model for both the controllers is one and the same and it is state controllable and observable. The h-infinitycontroller design is based on the selection of weighing function whereas the design of the LQR controller depends on theselection of optimal state feedback controller gain matrix. Performance comparison of both the controllers is carried out based on the settling time, peak overshoot and rise time. Simulation results show that h-infinity controller has bettersettling time compared to LQR controller.

Authors and Affiliations

Rajani S. H

Keywords

Related Articles

 Numerical Investigation of the Perfomance of Convergent Divergent Nozzle

 The main objective of the work is to analyse the performance and flow characteristics of convergent divergent nozzle and also to compare the numerical values of the two methods i.e “HIT & TRIAL METHOD” AND “A...

 Design, Simulation and Implementation of Flyback based, True Single Stage, Isolated, Power Factor Corrected AC-DC Converter for Solar Array Simulators

Presently most of the Power Factor correction circuits are based on boost topology. They consist of two  stages, one being the power factor correction (pre-regulator) and later DC-DC conversion stage. This paper pre...

 Applied lacunary interpolation for solving Boundary value problems

 Interpolation by various types of splines is the standard procedure in many applications. In this paper shall discuss the function, two and fourth derivatives of spline interpolation as an alternative to polynomial...

 Design of 8-Bit Comparator Using 45nm CMOS Technology

  In this paper design of 8- bit binary comparator using 45nm CMOS technology is discussed. This design needs less area and less number of transistors, also discussed about power and execution time. The circuit ha...

 Experimental study with different cathode and anode humidification temperatures in PEM fuel cell

 The paper gives experimental study and analysis of PEM Fuel cell with different humidification temperature. The paper focuses on the effect on the voltage and power obtained from fuel cell under variable humidifica...

Download PDF file
  • EP ID EP135825
  • DOI -
  • Views 106
  • Downloads 0

How To Cite

Rajani S. H (2013).  Performance Comparison of H-infinity and LQR Controllersfor the Pressure Regulation of a Hypersonic Wind Tunnel. International Journal of Modern Engineering Research (IJMER), 3(3), 1623-1629. https://europub.co.uk/articles/-A-135825