{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,3,23]],"date-time":"2026-03-23T12:05:56Z","timestamp":1774267556403,"version":"3.50.1"},"reference-count":43,"publisher":"Institute of Electrical and Electronics Engineers (IEEE)","license":[{"start":{"date-parts":[[2021,1,1]],"date-time":"2021-01-01T00:00:00Z","timestamp":1609459200000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/creativecommons.org\/licenses\/by\/4.0\/legalcode"}],"funder":[{"DOI":"10.13039\/501100001809","name":"Military Scientific Research Supports","doi-asserted-by":"publisher","award":["ZS2015070132A12012"],"award-info":[{"award-number":["ZS2015070132A12012"]}],"id":[{"id":"10.13039\/501100001809","id-type":"DOI","asserted-by":"publisher"}]}],"content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":["IEEE Access"],"published-print":{"date-parts":[[2021]]},"DOI":"10.1109\/access.2021.3052883","type":"journal-article","created":{"date-parts":[[2021,1,26]],"date-time":"2021-01-26T21:12:57Z","timestamp":1611695577000},"page":"15609-15622","source":"Crossref","is-referenced-by-count":5,"title":["Guidance Simulation and Experimental Verification of Trajectory Correction Mortar Projectile"],"prefix":"10.1109","volume":"9","author":[{"ORCID":"https:\/\/orcid.org\/0000-0001-7297-3264","authenticated-orcid":false,"given":"Xitong","family":"Sun","sequence":"first","affiliation":[],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Min","family":"Gao","sequence":"additional","affiliation":[],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Xiaodong","family":"Zhou","sequence":"additional","affiliation":[],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Jing","family":"Lv","sequence":"additional","affiliation":[],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Feng","family":"Tian","sequence":"additional","affiliation":[],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Zhiming","family":"Qiao","sequence":"additional","affiliation":[],"role":[{"role":"author","vocabulary":"crossref"}]}],"member":"263","reference":[{"key":"ref39","first-page":"22","article-title":"Dynamic threshold correction method of trajectory deviation based on perturbation theory","volume":"32","author":"wu","year":"2020","journal-title":"J Ballist"},{"key":"ref38","article-title":"Research on impact point prediction and control technology of trajectory correction rocket","author":"li","year":"2014"},{"key":"ref33","first-page":"2","author":"qian","year":"2016","journal-title":"Missile Flight Mechanics"},{"key":"ref32","doi-asserted-by":"publisher","DOI":"10.3182\/20120213-3-IN-4034.00031"},{"key":"ref31","doi-asserted-by":"publisher","DOI":"10.1109\/INDICON.2015.7443715"},{"key":"ref30","first-page":"190","article-title":"A new nonlinear guidance law formulation for proportional navigation guidance","author":"devan","year":"2012","journal-title":"Proc Int Workshop Variable Structure Syst"},{"key":"ref37","first-page":"97","article-title":"Braking control model and simulation for precision guided kit","volume":"36","author":"lu","year":"2016","journal-title":"Journal of Projectiles Rockets Missiles and Guidance"},{"key":"ref36","article-title":"Research theory and technology of flight control of the trajectory correction mortar projectile","author":"zhang","year":"2016"},{"key":"ref35","doi-asserted-by":"publisher","DOI":"10.1155\/2015\/781472"},{"key":"ref34","first-page":"23","author":"han","year":"2008","journal-title":"Exterior Ballistics"},{"key":"ref10","first-page":"195","article-title":"A biased proportional guidance algorithm for moving target with impact angle and field-of-view constraints","volume":"37","author":"huang","year":"2016","journal-title":"Astron J"},{"key":"ref40","doi-asserted-by":"publisher","DOI":"10.1155\/2015\/618458"},{"key":"ref11","first-page":"29","article-title":"Improvement of longitudinal trajectory-correction method based on perturbation theory","volume":"28","author":"gao","year":"2016","journal-title":"J Ballist"},{"key":"ref12","first-page":"86","article-title":"Impact point prediction algorithm based on perturbation theory","volume":"42","author":"tian","year":"2014","journal-title":"Modern Defence Technology"},{"key":"ref13","first-page":"1164","article-title":"Real-time impact point prediction of rocket projectile based on perturbation theory","volume":"35","author":"li","year":"2014","journal-title":"Acta Armamentarii"},{"key":"ref14","first-page":"52","article-title":"A guidance method for two dimensional trajectory correction projectile based on impact point prediction pf EKF","volume":"39","author":"pu","year":"2018","journal-title":"Journal of Ordnance Equipment Engineering"},{"key":"ref15","doi-asserted-by":"publisher","DOI":"10.1109\/SIU.2018.8404802"},{"key":"ref16","article-title":"Projectile impact point prediction based on self-propelled artillery dynamics and Doppler radar measurements","volume":"5","author":"khalil","year":"2015","journal-title":"Adv Mech Eng"},{"key":"ref17","doi-asserted-by":"publisher","DOI":"10.23919\/ICIF.2017.8009642"},{"key":"ref18","doi-asserted-by":"publisher","DOI":"10.2514\/1.59252"},{"key":"ref19","first-page":"29","article-title":"Initial value proportional navigation with impact angle constraint and overload constraint","volume":"39","author":"wang","year":"2019","journal-title":"Journal of Projectiles Rockets Missiles and Guidance"},{"key":"ref28","doi-asserted-by":"publisher","DOI":"10.2514\/1.37876"},{"key":"ref4","first-page":"67","article-title":"Development status and key technology of guided mortar shell","volume":"12","author":"zhu","year":"2016","journal-title":"Missile Aerodynamics"},{"key":"ref27","doi-asserted-by":"publisher","DOI":"10.2514\/1.8392"},{"key":"ref3","first-page":"56","article-title":"Development and key technologies of precision guidance module","volume":"12","author":"huang","year":"2016","journal-title":"Missile Aerodynamics"},{"key":"ref6","doi-asserted-by":"publisher","DOI":"10.2322\/tjsass.56.205"},{"key":"ref29","doi-asserted-by":"publisher","DOI":"10.2514\/1.37864"},{"key":"ref5","first-page":"81","article-title":"Development status and key technologies of two-dimensional ballistic correction components","volume":"14","author":"ke","year":"2018","journal-title":"Missile Aerodynamics"},{"key":"ref8","first-page":"815","article-title":"Terminal guidance control based on biased proportional navigation","volume":"25","author":"gao","year":"2017","journal-title":"J Chin Inertial Technol"},{"key":"ref7","first-page":"339","article-title":"New biased proportional guidance law application in air to ground combat","volume":"5","author":"mu","year":"2019","journal-title":"J Command Control"},{"key":"ref2","first-page":"127","article-title":"A summary for trajectory correction projectiles","volume":"31","author":"zhang","year":"2010","journal-title":"Acta Armamentarii"},{"key":"ref9","first-page":"2346","article-title":"Biased proportional navigation applicable for infrared guidance munitions","volume":"38","author":"wang","year":"2016","journal-title":"Syst Eng Electron"},{"key":"ref1","first-page":"24","article-title":"A review on development of foreign guided mortar projectile","volume":"32","author":"zhang","year":"2020","journal-title":"Journal of Projectiles Rockets Missiles and Guidance"},{"key":"ref20","first-page":"67","article-title":"Optimization design of proportional navigation guidance law with gravity over compensation based on guided projectile","volume":"38","author":"wang","year":"2017","journal-title":"Journal of Ordnance Equipment Engineering"},{"key":"ref22","doi-asserted-by":"publisher","DOI":"10.1109\/GNCC42960.2018.9019209"},{"key":"ref21","doi-asserted-by":"crossref","first-page":"277","DOI":"10.1109\/7.640285","article-title":"Biased PNG law for impact with angular constraint","volume":"34","author":"kim","year":"1998","journal-title":"IEEE Trans Aerosp Electron Syst"},{"key":"ref42","first-page":"347","article-title":"A practical adaptive proportional-derivative guidance law","volume":"24","author":"zhang","year":"2016","journal-title":"Eng Lett"},{"key":"ref24","doi-asserted-by":"publisher","DOI":"10.1109\/TAES.2019.2924175"},{"key":"ref41","first-page":"113","author":"siouris","year":"2004","journal-title":"Missile Guidance and Control Systems"},{"key":"ref23","doi-asserted-by":"publisher","DOI":"10.2514\/1.G005063.c1"},{"key":"ref26","first-page":"68","article-title":"BPNG law with arbitrary initial lead angle and terminal impact angle constraint and time-to-go estimation","volume":"40","author":"ma","year":"2019","journal-title":"Acta Armam"},{"key":"ref43","doi-asserted-by":"publisher","DOI":"10.1177\/1548512916647810"},{"key":"ref25","first-page":"29","article-title":"Guidance strategy with impact angle constraint based on pure proportional navigation","volume":"41","author":"li","year":"2020","journal-title":"Acta Aeronautica et Astronautica Sinica"}],"container-title":["IEEE Access"],"original-title":[],"link":[{"URL":"http:\/\/xplorestaging.ieee.org\/ielx7\/6287639\/9312710\/09328427.pdf?arnumber=9328427","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2021,12,17]],"date-time":"2021-12-17T19:56:18Z","timestamp":1639770978000},"score":1,"resource":{"primary":{"URL":"https:\/\/ieeexplore.ieee.org\/document\/9328427\/"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2021]]},"references-count":43,"URL":"https:\/\/doi.org\/10.1109\/access.2021.3052883","relation":{},"ISSN":["2169-3536"],"issn-type":[{"value":"2169-3536","type":"electronic"}],"subject":[],"published":{"date-parts":[[2021]]}}}