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The two-burn scheme is applied to eliminate velocity pointing error. Solutions for angular velocity, Euler angle, and inertial velocity with nonzero initial conditions are derived in a new form for axisymmetric spacecraft with constant mass. Simulations show that the solutions closely match numerical simulations and the two-burn scheme decrease the velocity pointing error obviously. Based on the solutions, the effect of two-burn scheme is analyzed. The results show that the spacecraft will obtain the minimum velocity pointing error if the burn and coast times are controlled accurately. Also, the two-burn scheme allows for a lower spin rate and the spacecraft can be maneuvered at nonzero initial conditions compared with the continuous thrust scheme.<\/jats:p>","DOI":"10.1177\/0142331219841106","type":"journal-article","created":{"date-parts":[[2019,5,10]],"date-time":"2019-05-10T02:13:22Z","timestamp":1557454402000},"page":"3877-3886","update-policy":"https:\/\/doi.org\/10.1177\/sage-journals-update-policy","source":"Crossref","is-referenced-by-count":1,"title":["Velocity pointing error reduction for symmetric spinning spacecraft via a two-burn scheme"],"prefix":"10.1177","volume":"41","author":[{"given":"Zhenhua","family":"Liang","sequence":"first","affiliation":[{"name":"School of Mechanical Engineering, Nanjing University of Science and Technology, China"}],"role":[{"role":"author","vocabulary":"crossref"}]},{"given":"Wenhe","family":"Liao","sequence":"additional","affiliation":[{"name":"School of Mechanical Engineering, Nanjing University of Science and 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