Data carrier where you saved the computer program for performing the method and the method of calculating rough orbit should be passed while being guided position

摘要

Set computer (15) (2) described by (AF) initial function, initial trajectory to be passed while the position guidance, thereby substituting initial function to (AF) (s) is the scalar trajectory parameter position corresponding initial trajectory of (2) on (pA) are defined respectively by. Unlike the time (t) is the scalar trajectory parameter (s), is characteristic for the (s) path proceeding along the initial trajectory (2). (15) initial trajectory as a function of the scalar trajectory parameter (s) in (2), is subjected to filtering with a low pass filter characteristic to target the scalar trajectory parameter (s), and then so rough function computer (GF) is obtained, and thereby, positions corresponding rough orbit (13) on the assignment (s) The scalar trajectory parameter to rough function (GF) (pG) is defined respectively. The computer (15), to always below the (S) limit it is preset without spacing rough trajectory to (13) are involved in the value scalar trajectory parameter (s) The initial trajectory (2) rough function (GF) I seek.