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METHOD FOR FORMING SIGNAL coordinates of the initial purpose of the object SIGHT AND PARAMETERS OF ITS INITIAL EXHIBITIONS AND INERTIAL Direction Finding System for implementing the method
METHOD FOR FORMING SIGNAL coordinates of the initial purpose of the object SIGHT AND PARAMETERS OF ITS INITIAL EXHIBITIONS AND INERTIAL Direction Finding System for implementing the method
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机译：形成物体初始目的信号坐标的方法及其初始展览的视线和参数以及实现该方法的惯性测向系统
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摘要
1. A method of forming coordinate signals initial sighting the target object and parameter conditions for the initial alignment of the inertial direction finding it, characterized in that during prelaunch movable carrier (CD) is determined and set signals proportional to the initial values of slant range, azimuth and inclination relative position PN and originally designated destination object of sight (S), wherein in the apparatus of preparation and launch control GON, external with respect to the claimed Images Retenu placed on a movable launch platform (SRP) form regular signals as a packet of successive information words, which contains initial values of the tilt angle and azimutanaznachennogo OB relative to the base of the integrated antenna device (AIO) mounted fixedly within the housing Mo, in a coordinate system related by weight Mo with the center, the slant range to the designated OS and an inclined closing velocity with SAPs vector projections linear velocity displacement prelaunch AIO base together with Mo, y tanovlenii on SRP, for respective axes of the local horizontal coordinate system of Cartesian coordinates Mo together with the SRP in the local horizontal coordinate system of yaw, pitch and roll Mo together with the base AIO and SRP, the longitude and latitude Mo together with SRP and furthermore signals required regime teams range forming algorithms integrated BSSN and desired trajectory PN motion control word and the control word; more generated signals in the form of successive information words package
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