Development of Automatic Firing Angle Calculation for Ground to Ground MLRS

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Development of Automatic Firing Angle Calculation for Ground to Ground MLRS

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dc.contributor.author Charubhun, Weerawut
dc.contributor.author Chusilp, Pawat
dc.date.accessioned 2563-08-25T03:41:13Z
dc.date.available 2563-08-25T03:41:13Z
dc.date.issued 2558
dc.identifier.uri http://hdl.handle.net/123456789/1927
dc.description บทความวิจัย en_US
dc.description.abstract This paper addresses a method to determine firing angles of an unguided ground to ground Multiple Launched Rocket System (MLRS). Six-degree of freedom trajectory simulation is used in prior to reveal all firing ranges of each firing angle and possible scenarios can be categorized. Some firing range can be achieved by two different firing angles while the others can be achieved by only one firing angle. By having prior knowledge of the firing ranges versus the firing angles, and by employing iterative binary search algorithm and six-degree of freedom trajectory calculation, the method to automatically and iteratively search for a firing angle corresponded to a specified firing range is formed. The method is tested with short range and medium range unguided ground to ground rockets at various firing condition. The results are presented and discussed. en_US
dc.description.sponsorship Defence Technology Institute en_US
dc.language.iso en en_US
dc.publisher Defence Technology Institute en_US
dc.relation.ispartofseries 58037;
dc.subject Fire control program en_US
dc.subject Trajectory sinmlation en_US
dc.subject Missile trajectory en_US
dc.subject Binary search en_US
dc.subject Firing tables en_US
dc.title Development of Automatic Firing Angle Calculation for Ground to Ground MLRS en_US
dc.type Article en_US


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