基本信息:
- 专利标题： A GENERALIZED PROCESS FOR ORDER REDUCTION OF UNSTABLE SYSTEMS
- 申请号：AU2020103941 申请日：2020-12-08
- 公开(公告)号：AU2020103941A4 公开(公告)日：2021-02-11
- 发明人： GANGULI SOUVIK , KARELIA NIRAV , CHANDRA PAL VIPIN , SINGH ARASHDEEP , SINGH MANJEET , SHARMA ADITI , SWARNAKAR JAYDEEP , SOHANE ANURAG , HANS SIKANDER
- 申请人： CHANDRA PAL VIPIN DR , GANGULI SOUVIK DR , HANS SIKANDER MR , KARELIA NIRAV MR , SHARMA ADITI DR , SINGH ARASHDEEP MR , SINGH MANJEET MR , SOHANE ANURAG MR , SWARNAKAR JAYDEEP DR
- 专利权人： CHANDRA PAL VIPIN DR,GANGULI SOUVIK DR,HANS SIKANDER MR,KARELIA NIRAV MR,SHARMA ADITI DR,SINGH ARASHDEEP MR,SINGH MANJEET MR,SOHANE ANURAG MR,SWARNAKAR JAYDEEP DR
- 当前专利权人： CHANDRA PAL VIPIN DR,GANGULI SOUVIK DR,HANS SIKANDER MR,KARELIA NIRAV MR,SHARMA ADITI DR,SINGH ARASHDEEP MR,SINGH MANJEET MR,SOHANE ANURAG MR,SWARNAKAR JAYDEEP DR
- 优先权： AU2020103941 2020-12-08
- 主分类号： G06F17/10
- IPC分类号： G06F17/10 ; B64C17/00 ; B64C19/00 ; G05B13/04 ; G05D1/02
摘要：
The present disclosure relates to a generalized process for order reduction of unstable systems. Plenty of engineering applications are often represented by complex, high-order models that are troublesome to analyze, control and design. Their reduced models are more appropriate to provide deep insight and can also contribute to design lower-order controllers. The main motive behind various model reduction techniques is to obtain an appropriate lower-order model such that it retains the input output behavior and inherent characteristics of the original system with reduced error. Thus, the multi-input multi-output model of highly maneuverable aircraft technology (HIMAT) has been reduced using a new pole shifting method. Finally, the controller of the reduced plant model is synthesized using an approximate model matching framework. Both model reduction and controller design problems are carried out using the delta operator. The delta domain approach unifies analysis of continuous and discrete-time systems at high sampling frequency. E oj cEr E) CLcc _0 Cfl 4-Uo 02 W '4 -0 C- 4 - 4 CL EUW Mci C)a ci)E E 4 WE a)) -o- E WoE V V- 4-'- + C 0 V> 4--2 '-C on W E on W -C WCU flE 4- 00 EE -64 W- W"04 Con 0) W'- 0 WE '4- 00> 0 0 0-W W 40 C> 4- 4- - 4- ~ 4- 0E 4t 4-CL V0 4- :--= - 414- E C EW c CL '4 C- 0 CW > C0' D4- 0 0 ;C