Continuous-Time Predictive Control-Based Integrated Guidance and Control
In this paper, a continuous-time predictive control-based novel integrated guidance and control formulation is proposed. Treating the target acceleration as a mismatched external disturbance, it is estimated along with the system states by means of a generalized extended state observer, and the esti...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Bhavnesh Panchal [verfasserIn] |
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| Format: |
Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2017 |
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| Schlagwörter: |
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| Übergeordnetes Werk: |
Enthalten in: Journal of guidance, control, and dynamics - New York, NY, 1982, 40(2017), 7, Seite 1579 |
|---|---|
| Übergeordnetes Werk: |
volume:40 ; year:2017 ; number:7 ; pages:1579 |
| Links: |
|---|
| DOI / URN: |
10.2514/1.G002661 |
|---|
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OLC1994259906 |
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| 520 | |a In this paper, a continuous-time predictive control-based novel integrated guidance and control formulation is proposed. Treating the target acceleration as a mismatched external disturbance, it is estimated along with the system states by means of a generalized extended state observer, and the estimates are used in the predictive design to make the latter implementable. Although the generalized extended state observer has robustified as well as addressed the need of a complete state vector in the predictive controller, the predictive control framework has offered a systematic approach for the design of the feedback control gain and disturbance compensation gain needed in the generalized extended state observer-based controller. Closed-loop stability of the overall system including the stability of internal dynamics is established. Simulation results including Monte Carlo simulation are presented to demonstrate the efficacy of the proposed integrated guidance and control law. The highlights of the formulation are that it is implementable using conventional seeker measurements; does not need any information about target maneuvers; caters to constraints on control inputs; and offers satisfactory performance for constant as well as varying missile velocities, stable as well as unstable configurations, and for different target acceleration profiles representative of highly maneuvering targets. | ||
| 650 | 4 | |a Monte Carlo simulation | |
| 650 | 4 | |a Compensation | |
| 650 | 4 | |a Control stability | |
| 650 | 4 | |a Control theory | |
| 650 | 4 | |a Simulation | |
| 650 | 4 | |a Monte Carlo method | |
| 650 | 4 | |a Acceleration | |
| 650 | 4 | |a Effectiveness | |
| 650 | 4 | |a Dynamics | |
| 650 | 4 | |a Maneuvering targets | |
| 650 | 4 | |a Estimates | |
| 650 | 4 | |a Computer simulation | |
| 650 | 4 | |a Design engineering | |
| 650 | 4 | |a Control systems | |
| 650 | 4 | |a Feedback control | |
| 650 | 4 | |a Dynamical systems | |
| 650 | 4 | |a Maneuvers | |
| 650 | 4 | |a Predictive control | |
| 650 | 4 | |a Feedback | |
| 650 | 4 | |a Dynamic stability | |
| 700 | 0 | |a Nilesh Mate |4 oth | |
| 700 | 0 | |a S E Talole |4 oth | |
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10.2514/1.G002661 doi PQ20170901 (DE-627)OLC1994259906 (DE-599)GBVOLC1994259906 (PRQ)proquest_journals_19093174460 (KEY)0032738720170000040000701579continuoustimepredictivecontrolbasedintegratedguid DE-627 ger DE-627 rakwb eng 380 DNB Bhavnesh Panchal verfasserin aut Continuous-Time Predictive Control-Based Integrated Guidance and Control 2017 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier In this paper, a continuous-time predictive control-based novel integrated guidance and control formulation is proposed. Treating the target acceleration as a mismatched external disturbance, it is estimated along with the system states by means of a generalized extended state observer, and the estimates are used in the predictive design to make the latter implementable. Although the generalized extended state observer has robustified as well as addressed the need of a complete state vector in the predictive controller, the predictive control framework has offered a systematic approach for the design of the feedback control gain and disturbance compensation gain needed in the generalized extended state observer-based controller. Closed-loop stability of the overall system including the stability of internal dynamics is established. Simulation results including Monte Carlo simulation are presented to demonstrate the efficacy of the proposed integrated guidance and control law. The highlights of the formulation are that it is implementable using conventional seeker measurements; does not need any information about target maneuvers; caters to constraints on control inputs; and offers satisfactory performance for constant as well as varying missile velocities, stable as well as unstable configurations, and for different target acceleration profiles representative of highly maneuvering targets. Monte Carlo simulation Compensation Control stability Control theory Simulation Monte Carlo method Acceleration Effectiveness Dynamics Maneuvering targets Estimates Computer simulation Design engineering Control systems Feedback control Dynamical systems Maneuvers Predictive control Feedback Dynamic stability Nilesh Mate oth S E Talole oth Enthalten in Journal of guidance, control, and dynamics New York, NY, 1982 40(2017), 7, Seite 1579 (DE-627)130551910 (DE-600)782987-5 (DE-576)016107497 0731-5090 nnns volume:40 year:2017 number:7 pages:1579 http://dx.doi.org/10.2514/1.G002661 Volltext https://search.proquest.com/docview/1909317446 GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_70 GBV_ILN_4046 GBV_ILN_4700 AR 40 2017 7 1579 |
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10.2514/1.G002661 doi PQ20170901 (DE-627)OLC1994259906 (DE-599)GBVOLC1994259906 (PRQ)proquest_journals_19093174460 (KEY)0032738720170000040000701579continuoustimepredictivecontrolbasedintegratedguid DE-627 ger DE-627 rakwb eng 380 DNB Bhavnesh Panchal verfasserin aut Continuous-Time Predictive Control-Based Integrated Guidance and Control 2017 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier In this paper, a continuous-time predictive control-based novel integrated guidance and control formulation is proposed. Treating the target acceleration as a mismatched external disturbance, it is estimated along with the system states by means of a generalized extended state observer, and the estimates are used in the predictive design to make the latter implementable. Although the generalized extended state observer has robustified as well as addressed the need of a complete state vector in the predictive controller, the predictive control framework has offered a systematic approach for the design of the feedback control gain and disturbance compensation gain needed in the generalized extended state observer-based controller. Closed-loop stability of the overall system including the stability of internal dynamics is established. Simulation results including Monte Carlo simulation are presented to demonstrate the efficacy of the proposed integrated guidance and control law. The highlights of the formulation are that it is implementable using conventional seeker measurements; does not need any information about target maneuvers; caters to constraints on control inputs; and offers satisfactory performance for constant as well as varying missile velocities, stable as well as unstable configurations, and for different target acceleration profiles representative of highly maneuvering targets. Monte Carlo simulation Compensation Control stability Control theory Simulation Monte Carlo method Acceleration Effectiveness Dynamics Maneuvering targets Estimates Computer simulation Design engineering Control systems Feedback control Dynamical systems Maneuvers Predictive control Feedback Dynamic stability Nilesh Mate oth S E Talole oth Enthalten in Journal of guidance, control, and dynamics New York, NY, 1982 40(2017), 7, Seite 1579 (DE-627)130551910 (DE-600)782987-5 (DE-576)016107497 0731-5090 nnns volume:40 year:2017 number:7 pages:1579 http://dx.doi.org/10.2514/1.G002661 Volltext https://search.proquest.com/docview/1909317446 GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_70 GBV_ILN_4046 GBV_ILN_4700 AR 40 2017 7 1579 |
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10.2514/1.G002661 doi PQ20170901 (DE-627)OLC1994259906 (DE-599)GBVOLC1994259906 (PRQ)proquest_journals_19093174460 (KEY)0032738720170000040000701579continuoustimepredictivecontrolbasedintegratedguid DE-627 ger DE-627 rakwb eng 380 DNB Bhavnesh Panchal verfasserin aut Continuous-Time Predictive Control-Based Integrated Guidance and Control 2017 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier In this paper, a continuous-time predictive control-based novel integrated guidance and control formulation is proposed. Treating the target acceleration as a mismatched external disturbance, it is estimated along with the system states by means of a generalized extended state observer, and the estimates are used in the predictive design to make the latter implementable. Although the generalized extended state observer has robustified as well as addressed the need of a complete state vector in the predictive controller, the predictive control framework has offered a systematic approach for the design of the feedback control gain and disturbance compensation gain needed in the generalized extended state observer-based controller. Closed-loop stability of the overall system including the stability of internal dynamics is established. Simulation results including Monte Carlo simulation are presented to demonstrate the efficacy of the proposed integrated guidance and control law. The highlights of the formulation are that it is implementable using conventional seeker measurements; does not need any information about target maneuvers; caters to constraints on control inputs; and offers satisfactory performance for constant as well as varying missile velocities, stable as well as unstable configurations, and for different target acceleration profiles representative of highly maneuvering targets. Monte Carlo simulation Compensation Control stability Control theory Simulation Monte Carlo method Acceleration Effectiveness Dynamics Maneuvering targets Estimates Computer simulation Design engineering Control systems Feedback control Dynamical systems Maneuvers Predictive control Feedback Dynamic stability Nilesh Mate oth S E Talole oth Enthalten in Journal of guidance, control, and dynamics New York, NY, 1982 40(2017), 7, Seite 1579 (DE-627)130551910 (DE-600)782987-5 (DE-576)016107497 0731-5090 nnns volume:40 year:2017 number:7 pages:1579 http://dx.doi.org/10.2514/1.G002661 Volltext https://search.proquest.com/docview/1909317446 GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_70 GBV_ILN_4046 GBV_ILN_4700 AR 40 2017 7 1579 |
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10.2514/1.G002661 doi PQ20170901 (DE-627)OLC1994259906 (DE-599)GBVOLC1994259906 (PRQ)proquest_journals_19093174460 (KEY)0032738720170000040000701579continuoustimepredictivecontrolbasedintegratedguid DE-627 ger DE-627 rakwb eng 380 DNB Bhavnesh Panchal verfasserin aut Continuous-Time Predictive Control-Based Integrated Guidance and Control 2017 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier In this paper, a continuous-time predictive control-based novel integrated guidance and control formulation is proposed. Treating the target acceleration as a mismatched external disturbance, it is estimated along with the system states by means of a generalized extended state observer, and the estimates are used in the predictive design to make the latter implementable. Although the generalized extended state observer has robustified as well as addressed the need of a complete state vector in the predictive controller, the predictive control framework has offered a systematic approach for the design of the feedback control gain and disturbance compensation gain needed in the generalized extended state observer-based controller. Closed-loop stability of the overall system including the stability of internal dynamics is established. Simulation results including Monte Carlo simulation are presented to demonstrate the efficacy of the proposed integrated guidance and control law. The highlights of the formulation are that it is implementable using conventional seeker measurements; does not need any information about target maneuvers; caters to constraints on control inputs; and offers satisfactory performance for constant as well as varying missile velocities, stable as well as unstable configurations, and for different target acceleration profiles representative of highly maneuvering targets. Monte Carlo simulation Compensation Control stability Control theory Simulation Monte Carlo method Acceleration Effectiveness Dynamics Maneuvering targets Estimates Computer simulation Design engineering Control systems Feedback control Dynamical systems Maneuvers Predictive control Feedback Dynamic stability Nilesh Mate oth S E Talole oth Enthalten in Journal of guidance, control, and dynamics New York, NY, 1982 40(2017), 7, Seite 1579 (DE-627)130551910 (DE-600)782987-5 (DE-576)016107497 0731-5090 nnns volume:40 year:2017 number:7 pages:1579 http://dx.doi.org/10.2514/1.G002661 Volltext https://search.proquest.com/docview/1909317446 GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_70 GBV_ILN_4046 GBV_ILN_4700 AR 40 2017 7 1579 |
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10.2514/1.G002661 doi PQ20170901 (DE-627)OLC1994259906 (DE-599)GBVOLC1994259906 (PRQ)proquest_journals_19093174460 (KEY)0032738720170000040000701579continuoustimepredictivecontrolbasedintegratedguid DE-627 ger DE-627 rakwb eng 380 DNB Bhavnesh Panchal verfasserin aut Continuous-Time Predictive Control-Based Integrated Guidance and Control 2017 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier In this paper, a continuous-time predictive control-based novel integrated guidance and control formulation is proposed. Treating the target acceleration as a mismatched external disturbance, it is estimated along with the system states by means of a generalized extended state observer, and the estimates are used in the predictive design to make the latter implementable. Although the generalized extended state observer has robustified as well as addressed the need of a complete state vector in the predictive controller, the predictive control framework has offered a systematic approach for the design of the feedback control gain and disturbance compensation gain needed in the generalized extended state observer-based controller. Closed-loop stability of the overall system including the stability of internal dynamics is established. Simulation results including Monte Carlo simulation are presented to demonstrate the efficacy of the proposed integrated guidance and control law. The highlights of the formulation are that it is implementable using conventional seeker measurements; does not need any information about target maneuvers; caters to constraints on control inputs; and offers satisfactory performance for constant as well as varying missile velocities, stable as well as unstable configurations, and for different target acceleration profiles representative of highly maneuvering targets. Monte Carlo simulation Compensation Control stability Control theory Simulation Monte Carlo method Acceleration Effectiveness Dynamics Maneuvering targets Estimates Computer simulation Design engineering Control systems Feedback control Dynamical systems Maneuvers Predictive control Feedback Dynamic stability Nilesh Mate oth S E Talole oth Enthalten in Journal of guidance, control, and dynamics New York, NY, 1982 40(2017), 7, Seite 1579 (DE-627)130551910 (DE-600)782987-5 (DE-576)016107497 0731-5090 nnns volume:40 year:2017 number:7 pages:1579 http://dx.doi.org/10.2514/1.G002661 Volltext https://search.proquest.com/docview/1909317446 GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_70 GBV_ILN_4046 GBV_ILN_4700 AR 40 2017 7 1579 |
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Enthalten in Journal of guidance, control, and dynamics 40(2017), 7, Seite 1579 volume:40 year:2017 number:7 pages:1579 |
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Continuous-Time Predictive Control-Based Integrated Guidance and Control |
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Continuous-Time Predictive Control-Based Integrated Guidance and Control |
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Bhavnesh Panchal |
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continuous-time predictive control-based integrated guidance and control |
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Continuous-Time Predictive Control-Based Integrated Guidance and Control |
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In this paper, a continuous-time predictive control-based novel integrated guidance and control formulation is proposed. Treating the target acceleration as a mismatched external disturbance, it is estimated along with the system states by means of a generalized extended state observer, and the estimates are used in the predictive design to make the latter implementable. Although the generalized extended state observer has robustified as well as addressed the need of a complete state vector in the predictive controller, the predictive control framework has offered a systematic approach for the design of the feedback control gain and disturbance compensation gain needed in the generalized extended state observer-based controller. Closed-loop stability of the overall system including the stability of internal dynamics is established. Simulation results including Monte Carlo simulation are presented to demonstrate the efficacy of the proposed integrated guidance and control law. The highlights of the formulation are that it is implementable using conventional seeker measurements; does not need any information about target maneuvers; caters to constraints on control inputs; and offers satisfactory performance for constant as well as varying missile velocities, stable as well as unstable configurations, and for different target acceleration profiles representative of highly maneuvering targets. |
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In this paper, a continuous-time predictive control-based novel integrated guidance and control formulation is proposed. Treating the target acceleration as a mismatched external disturbance, it is estimated along with the system states by means of a generalized extended state observer, and the estimates are used in the predictive design to make the latter implementable. Although the generalized extended state observer has robustified as well as addressed the need of a complete state vector in the predictive controller, the predictive control framework has offered a systematic approach for the design of the feedback control gain and disturbance compensation gain needed in the generalized extended state observer-based controller. Closed-loop stability of the overall system including the stability of internal dynamics is established. Simulation results including Monte Carlo simulation are presented to demonstrate the efficacy of the proposed integrated guidance and control law. The highlights of the formulation are that it is implementable using conventional seeker measurements; does not need any information about target maneuvers; caters to constraints on control inputs; and offers satisfactory performance for constant as well as varying missile velocities, stable as well as unstable configurations, and for different target acceleration profiles representative of highly maneuvering targets. |
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In this paper, a continuous-time predictive control-based novel integrated guidance and control formulation is proposed. Treating the target acceleration as a mismatched external disturbance, it is estimated along with the system states by means of a generalized extended state observer, and the estimates are used in the predictive design to make the latter implementable. Although the generalized extended state observer has robustified as well as addressed the need of a complete state vector in the predictive controller, the predictive control framework has offered a systematic approach for the design of the feedback control gain and disturbance compensation gain needed in the generalized extended state observer-based controller. Closed-loop stability of the overall system including the stability of internal dynamics is established. Simulation results including Monte Carlo simulation are presented to demonstrate the efficacy of the proposed integrated guidance and control law. The highlights of the formulation are that it is implementable using conventional seeker measurements; does not need any information about target maneuvers; caters to constraints on control inputs; and offers satisfactory performance for constant as well as varying missile velocities, stable as well as unstable configurations, and for different target acceleration profiles representative of highly maneuvering targets. |
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Continuous-Time Predictive Control-Based Integrated Guidance and Control |
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