发明名称 LAUNCH CONTROL SYSTEM FOR FLIGHT TEST
摘要 PURPOSE: A launch control system for a flight test is provided to process control information into various kinds of communication protocols and messages, thereby improving a control function for a guided weapon flight test, and processing various kinds of control signals. CONSTITUTION: A launch control system for a flight test includes a launch control signal processor(130), a system controller(110), a remote controller(160), a control signal distributor(150), a status indicator(140), and a shoot control system(120). The launch control signal processor implements launch control signal transmission/reception, signal treatment, and communication protocol conversion for a target flight vehicle. The system controller manages the entire launch control system including the launch control signal processor, and controls linked equipment. The remote controller interfaces with the shoot control system of a remote location. The control signal distributor interfaces with communication signals between the launch control signal processor and the remote controller. The status indicator indicates launch control information from the control signal distributor, and generates event information, and then transmits the event information to the launch control signal processor. The shoot control system linked with the launch control system for the flight test controls launching procedures for a guided missile through an interface with the launch control signal processor and the control signal distributor. [Reference numerals] (110) System controller; (120) Shoot control system; (130) Launch control signal processor; (140) Status indicator; (150) Control signal distributor; (160) Remote controller; (170) Flight test control computer; (180) Visual countdown device
申请公布号 KR20130019561(A) 申请公布日期 2013.02.27
申请号 KR20110081577 申请日期 2011.08.17
申请人 AGENCY FOR DEFENSE DEVELOPMENT 发明人 MIN, JOON KI;LEE, JAE YOB;BAEK, JEONG BU;LEE, YONG JAE
分类号 F42B15/01;F41G3/32;F41G7/30;G05D1/00 主分类号 F42B15/01
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