{"id":13292,"date":"2014-10-22T05:33:01","date_gmt":"2014-10-22T05:33:01","guid":{"rendered":"http:\/\/faculty.washington.edu\/chx\/?post_type=publication&#038;p=13292"},"modified":"2019-10-29T22:47:16","modified_gmt":"2019-10-29T22:47:16","slug":"adaptive-sliding-mode-spacecraft-attitude-control","status":"publish","type":"publication","link":"https:\/\/depts.washington.edu\/xchenlab\/publication\/adaptive-sliding-mode-spacecraft-attitude-control\/","title":{"rendered":"Adaptive sliding mode spacecraft attitude control"},"content":{"rendered":"\n<p>an adaptive sliding mode spacecraft attitude controller, has the advantage of not requiring knowledge of the inertia of the spacecraft, and rejecting unexpected external disturbances, with global asymptotic position and velocity tracking<\/p>\n","protected":false},"author":5,"featured_media":0,"template":"","meta":{"spay_email":""},"categories":[236],"jetpack_sharing_enabled":true,"jetpack_likes_enabled":false,"_links":{"self":[{"href":"https:\/\/depts.washington.edu\/xchenlab\/wp-json\/wp\/v2\/publication\/13292"}],"collection":[{"href":"https:\/\/depts.washington.edu\/xchenlab\/wp-json\/wp\/v2\/publication"}],"about":[{"href":"https:\/\/depts.washington.edu\/xchenlab\/wp-json\/wp\/v2\/types\/publication"}],"author":[{"embeddable":true,"href":"https:\/\/depts.washington.edu\/xchenlab\/wp-json\/wp\/v2\/users\/5"}],"wp:attachment":[{"href":"https:\/\/depts.washington.edu\/xchenlab\/wp-json\/wp\/v2\/media?parent=13292"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/depts.washington.edu\/xchenlab\/wp-json\/wp\/v2\/categories?post=13292"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}