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Dynamic characteristics analysis of missile in ballistic flight
In this research, the nonlinear model of a ballistic missile has been linearized and validated. The nonlinear equation of motion for the flight dynamics of the missile has been used for modeling the missile. The transfer function and model reduction are derived. Dynamic stability analysis for longit...
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creator | Audric, Derren Fayyadh, M. S. Dzaki Sembiring, Javensius Putro, Idris Eko |
description | In this research, the nonlinear model of a ballistic missile has been linearized and validated. The nonlinear equation of motion for the flight dynamics of the missile has been used for modeling the missile. The transfer function and model reduction are derived. Dynamic stability analysis for longitudinal and lateral-directional motion has been made at some operating points throughout the flight. The effect of different phases and velocities of the flight has been analyzed by its pole locations and frequency response. It was found that the missile’s short period, Dutch roll, and roll subsidence mode are stable. The result of this work can be used for designing a robust autopilot controller that meets the stability and performance requirements of the plant throughout the whole flight envelope. |
doi_str_mv | 10.1063/5.0182689 |
format | conference_proceeding |
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S. Dzaki ; Sembiring, Javensius ; Putro, Idris Eko</creator><contributor>Sitompul, Peberlin Parulian ; Muhamad, Johan ; Santosa, Cahya Edi ; Batubara, Mario ; Restasari, Afni ; Vetrita, Yenni ; Fitrianingsih, Ery ; Abadi, Prayitno ; Septanto, Harry ; Adhynugraha, Muhammad Ilham ; Yulihastin, Erma ; Mardianis</contributor><creatorcontrib>Audric, Derren ; Fayyadh, M. S. Dzaki ; Sembiring, Javensius ; Putro, Idris Eko ; Sitompul, Peberlin Parulian ; Muhamad, Johan ; Santosa, Cahya Edi ; Batubara, Mario ; Restasari, Afni ; Vetrita, Yenni ; Fitrianingsih, Ery ; Abadi, Prayitno ; Septanto, Harry ; Adhynugraha, Muhammad Ilham ; Yulihastin, Erma ; Mardianis</creatorcontrib><description>In this research, the nonlinear model of a ballistic missile has been linearized and validated. The nonlinear equation of motion for the flight dynamics of the missile has been used for modeling the missile. The transfer function and model reduction are derived. Dynamic stability analysis for longitudinal and lateral-directional motion has been made at some operating points throughout the flight. The effect of different phases and velocities of the flight has been analyzed by its pole locations and frequency response. It was found that the missile’s short period, Dutch roll, and roll subsidence mode are stable. The result of this work can be used for designing a robust autopilot controller that meets the stability and performance requirements of the plant throughout the whole flight envelope.</description><identifier>ISSN: 0094-243X</identifier><identifier>EISSN: 1551-7616</identifier><identifier>DOI: 10.1063/5.0182689</identifier><identifier>CODEN: APCPCS</identifier><language>eng</language><publisher>Melville: American Institute of Physics</publisher><subject>Automatic pilots ; Ballistic missiles ; Dynamic characteristics ; Dynamic stability ; Equations of motion ; Flight envelopes ; Frequency response ; Lateral stability ; Longitudinal stability ; Model reduction ; Motion stability ; Nonlinear equations ; Robust control ; Stability analysis ; Transfer functions</subject><ispartof>AIP conference proceedings, 2023, Vol.2941 (1)</ispartof><rights>Author(s)</rights><rights>2023 Author(s). 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Dzaki</creatorcontrib><creatorcontrib>Sembiring, Javensius</creatorcontrib><creatorcontrib>Putro, Idris Eko</creatorcontrib><title>Dynamic characteristics analysis of missile in ballistic flight</title><title>AIP conference proceedings</title><description>In this research, the nonlinear model of a ballistic missile has been linearized and validated. The nonlinear equation of motion for the flight dynamics of the missile has been used for modeling the missile. The transfer function and model reduction are derived. Dynamic stability analysis for longitudinal and lateral-directional motion has been made at some operating points throughout the flight. The effect of different phases and velocities of the flight has been analyzed by its pole locations and frequency response. It was found that the missile’s short period, Dutch roll, and roll subsidence mode are stable. The result of this work can be used for designing a robust autopilot controller that meets the stability and performance requirements of the plant throughout the whole flight envelope.</description><subject>Automatic pilots</subject><subject>Ballistic missiles</subject><subject>Dynamic characteristics</subject><subject>Dynamic stability</subject><subject>Equations of motion</subject><subject>Flight envelopes</subject><subject>Frequency response</subject><subject>Lateral stability</subject><subject>Longitudinal stability</subject><subject>Model reduction</subject><subject>Motion stability</subject><subject>Nonlinear equations</subject><subject>Robust control</subject><subject>Stability analysis</subject><subject>Transfer functions</subject><issn>0094-243X</issn><issn>1551-7616</issn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2023</creationdate><recordtype>conference_proceeding</recordtype><recordid>eNotkEtLxDAUhYMoWEcX_oOAO6HjzbPNSmR8woAbBXfhNk2dDH3ZZBbz763OrM7ifBw-DiHXDJYMtLhTS2Al16U5IRlTiuWFZvqUZABG5lyKr3NyEeMWgJuiKDNy_7jvsQuOug1O6JKfQkzBRYo9tvsYIh0a2oUYQ-tp6GmFbftP0KYN35t0Sc4abKO_OuaCfD4_faxe8_X7y9vqYZ2PTIiUY-UMK0ShXc05Y9ogh8pUBlBJqUptnNRMoi9rnFvna1c7VOCr2rhKz94LcnPYHafhZ-djstthN82O0XIDILkopZip2wMVXUiYwtDbcQodTnvLwP4dZJU9HiR-Ab7qV6U</recordid><startdate>20231211</startdate><enddate>20231211</enddate><creator>Audric, Derren</creator><creator>Fayyadh, M. S. Dzaki</creator><creator>Sembiring, Javensius</creator><creator>Putro, Idris Eko</creator><general>American Institute of Physics</general><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20231211</creationdate><title>Dynamic characteristics analysis of missile in ballistic flight</title><author>Audric, Derren ; Fayyadh, M. S. 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Dzaki</creatorcontrib><creatorcontrib>Sembiring, Javensius</creatorcontrib><creatorcontrib>Putro, Idris Eko</creatorcontrib><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Audric, Derren</au><au>Fayyadh, M. S. Dzaki</au><au>Sembiring, Javensius</au><au>Putro, Idris Eko</au><au>Sitompul, Peberlin Parulian</au><au>Muhamad, Johan</au><au>Santosa, Cahya Edi</au><au>Batubara, Mario</au><au>Restasari, Afni</au><au>Vetrita, Yenni</au><au>Fitrianingsih, Ery</au><au>Abadi, Prayitno</au><au>Septanto, Harry</au><au>Adhynugraha, Muhammad Ilham</au><au>Yulihastin, Erma</au><au>Mardianis</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Dynamic characteristics analysis of missile in ballistic flight</atitle><btitle>AIP conference proceedings</btitle><date>2023-12-11</date><risdate>2023</risdate><volume>2941</volume><issue>1</issue><issn>0094-243X</issn><eissn>1551-7616</eissn><coden>APCPCS</coden><abstract>In this research, the nonlinear model of a ballistic missile has been linearized and validated. The nonlinear equation of motion for the flight dynamics of the missile has been used for modeling the missile. The transfer function and model reduction are derived. Dynamic stability analysis for longitudinal and lateral-directional motion has been made at some operating points throughout the flight. The effect of different phases and velocities of the flight has been analyzed by its pole locations and frequency response. It was found that the missile’s short period, Dutch roll, and roll subsidence mode are stable. The result of this work can be used for designing a robust autopilot controller that meets the stability and performance requirements of the plant throughout the whole flight envelope.</abstract><cop>Melville</cop><pub>American Institute of Physics</pub><doi>10.1063/5.0182689</doi><tpages>10</tpages></addata></record> |
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source | American Institute of Physics:Jisc Collections:Transitional Journals Agreement 2021-23 (Reading list) |
subjects | Automatic pilots Ballistic missiles Dynamic characteristics Dynamic stability Equations of motion Flight envelopes Frequency response Lateral stability Longitudinal stability Model reduction Motion stability Nonlinear equations Robust control Stability analysis Transfer functions |
title | Dynamic characteristics analysis of missile in ballistic flight |
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