{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2025,2,21]],"date-time":"2025-02-21T01:03:22Z","timestamp":1740099802710,"version":"3.37.3"},"reference-count":18,"publisher":"IEEE","license":[{"start":{"date-parts":[[2020,10,9]],"date-time":"2020-10-09T00:00:00Z","timestamp":1602201600000},"content-version":"vor","delay-in-days":0,"URL":"https:\/\/ieeexplore.ieee.org\/Xplorehelp\/downloads\/license-information\/IEEE.html"},{"start":{"date-parts":[[2020,10,9]],"date-time":"2020-10-09T00:00:00Z","timestamp":1602201600000},"content-version":"stm-asf","delay-in-days":0,"URL":"https:\/\/doi.org\/10.15223\/policy-029"},{"start":{"date-parts":[[2020,10,9]],"date-time":"2020-10-09T00:00:00Z","timestamp":1602201600000},"content-version":"stm-asf","delay-in-days":0,"URL":"https:\/\/doi.org\/10.15223\/policy-037"}],"funder":[{"DOI":"10.13039\/501100001809","name":"National Natural Science Foundation of China","doi-asserted-by":"publisher","id":[{"id":"10.13039\/501100001809","id-type":"DOI","asserted-by":"publisher"}]}],"content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":[],"published-print":{"date-parts":[[2020,10,9]]},"DOI":"10.1109\/icca51439.2020.9264583","type":"proceedings-article","created":{"date-parts":[[2020,11,30]],"date-time":"2020-11-30T21:36:44Z","timestamp":1606772204000},"page":"1199-1204","source":"Crossref","is-referenced-by-count":0,"title":["Three-Dimensional Trajectory Optimization for soft lunar landing considering landing constraints"],"prefix":"10.1109","author":[{"given":"Yandi","family":"Qiao","sequence":"first","affiliation":[]},{"given":"Zexu","family":"Zhang","sequence":"additional","affiliation":[]},{"given":"Feng","family":"Chen","sequence":"additional","affiliation":[]},{"given":"Xingyan","family":"Wang","sequence":"additional","affiliation":[]},{"given":"Jing","family":"Wang","sequence":"additional","affiliation":[]}],"member":"263","reference":[{"key":"ref10","doi-asserted-by":"publisher","DOI":"10.1016\/j.asr.2019.12.030"},{"key":"ref11","article-title":"Research of Optimal Control Strategy Based on Multiple Shooting with Time Grid Refinement","author":"xiangyu","year":"2017","journal-title":"M S thesis"},{"key":"ref12","doi-asserted-by":"publisher","DOI":"10.3182\/20100906-5-JP-2022.00031"},{"key":"ref13","article-title":"Optimization of descent trajectories for lunar base settlement","author":"boere","year":"2010","journal-title":"M S thesis"},{"key":"ref14","doi-asserted-by":"publisher","DOI":"10.2514\/1.1329"},{"key":"ref15","first-page":"76","article-title":"On certain questions in the theory of optimal control","volume":"1","author":"filippov","year":"2006","journal-title":"Journal of the Society for Industrial & Applied Mathematics"},{"key":"ref16","first-page":"37","article-title":"A Necessary Conditions for the Existence and Sufficient Conditions for the Nonexistence of Solutions to a Certain Fractional Telegraph Equation","volume":"56","author":"berbiche","year":"2012","journal-title":"Memoirs Differential Equations and Mathematics Physics"},{"key":"ref17","doi-asserted-by":"publisher","DOI":"10.1109\/AERO.2003.1235204"},{"key":"ref18","first-page":"27","article-title":"On-board optimal nominal trajectory guidance method for lunar pinpoint soft landing","volume":"31","author":"liang","year":"2011","journal-title":"Chinese Space Science and Technology"},{"key":"ref4","article-title":"Switching System Model for Pinpoint Lunar Landing Guidance Using a Hybrid Control Strategy","author":"wibben","year":"2013","journal-title":"AIAA Guidance Navigation & Control Conference"},{"key":"ref3","doi-asserted-by":"publisher","DOI":"10.2514\/1.G004549"},{"key":"ref6","doi-asserted-by":"publisher","DOI":"10.1016\/j.advengsoft.2016.08.002"},{"key":"ref5","article-title":"Lunar Landing Simulation","author":"filo","year":"2019","journal-title":"Bachelor-Thesis"},{"key":"ref8","doi-asserted-by":"publisher","DOI":"10.2514\/6.2013-5258"},{"key":"ref7","doi-asserted-by":"publisher","DOI":"10.2514\/1.43024"},{"key":"ref2","doi-asserted-by":"publisher","DOI":"10.2514\/6.2019-0668"},{"key":"ref1","article-title":"Rapid Lunar Soft-Landing Trajectory Optimization by a Legendre Pseudospectral Method","author":"luo","year":"2012","journal-title":"presented at the 57th International Astronautical Congress"},{"key":"ref9","article-title":"Constrained Trajectory Optimization of a Soft Lunar Landing from a Parking Orbit","author":"hawkins","year":"2005","journal-title":"M S thesis"}],"event":{"name":"2020 IEEE 16th International Conference on Control & Automation (ICCA)","start":{"date-parts":[[2020,10,9]]},"location":"Singapore","end":{"date-parts":[[2020,10,11]]}},"container-title":["2020 IEEE 16th International Conference on Control & Automation (ICCA)"],"original-title":[],"link":[{"URL":"http:\/\/xplorestaging.ieee.org\/ielx7\/9264304\/9264308\/09264583.pdf?arnumber=9264583","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2022,6,28]],"date-time":"2022-06-28T00:16:23Z","timestamp":1656375383000},"score":1,"resource":{"primary":{"URL":"https:\/\/ieeexplore.ieee.org\/document\/9264583\/"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2020,10,9]]},"references-count":18,"URL":"https:\/\/doi.org\/10.1109\/icca51439.2020.9264583","relation":{},"subject":[],"published":{"date-parts":[[2020,10,9]]}}}