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专刊的详细说明:本专刊系有关采用自动搜索跟踪装置的时间调节器高精度地控制位置的制导飞行器装置。作为飞行器的制导方式有复合制导方式。该方式是发射后的飞行器初始无制导或采用惯性制导,而至后期使目标搜索跟踪装置工作,并搜索跟踪目标。为使上述的目标搜索跟踪装置工作,在发射飞行器之前,首先要调整时间调节器,次确定搜索目标的初始位置。一般地目标搜索跟踪装置,搜索范围的角度及其距离的有限制。为此,如图1所示,在飞行器的推力,即速度误差很大时,即使开始搜索目标,然而,在其搜索范围内(图中的斜线部分)也可能不存在目标。图1a 所示的是,当飞行器 M 的推力与予定的推力一致时,到达搜索开始的予定地点,在其搜索范围 R 内捕获目标 TGT 的情形。另
Detailed Description of the Special Issue: This special issue relates to a guided aircraft device that uses a time regulator of an automatic search and tracking device to control the position with high accuracy. As the guidance of the aircraft complex guidance system. This is the initial launch of the aircraft without guidance or inertial guidance, and later to make the target search tracking device work, and search tracking target. In order to make the target tracking device work, before launching an aircraft, the time regulator needs to be adjusted first to determine the initial position of the search target. In general, target search tracking devices have limitations on the search range and their distance. For this reason, as shown in FIG. 1, when the thrust of the aircraft, that is, the speed error is large, the target may not exist even within the search range (hatched portion in the figure) even if the search for the target is started. Fig. 1a shows the case where the target TGT is captured within its search range R when the thrust of the aircraft M coincides with a predetermined thrust, reaching a predetermined point at the beginning of the search. another