The missile already has some orientation capability meant for flying inside the beam that the launching platform is using to illuminate the target. Line-of-sight beam riding guidance (LOSBR) - The target tracker is on board the missile.These missiles are totally controlled by the launching platform that sends all control orders to the missile. Command guidance - The missile tracker is on the launching platform.These guidance systems usually need the use of radars and a radio or wired link between the control point and the missile in other words, the trajectory is controlled with the information transmitted via radio or wire (see Wire-guided missile). Homing guidance: The guidance computers are in the missile and in the target tracker.The target tracker is also placed on the launching platform. Remote control guidance: The guidance computer is on the launcher.The way these three subsystems are distributed between the missile and the launcher result in two different categories: In every go-onto-target system there are three subsystems: ( December 2016) ( Learn how and when to remove this template message) Unsourced material may be challenged and removed. Please help improve this article by adding citations to reliable sources. This section needs additional citations for verification. In GOLIS systems, the problem is simpler because the target is not moving. The target needs to be eliminated in a timely fashion in order to preserve the integrity of the sender. Also, a moving target can be an immediate threat to the sender of the missile. The trajectory that a missile takes while attacking a moving target is dependent upon the movement of the target. A GOT missile can target either a moving or fixed target, whereas a GOLIS weapon is limited to a stationary or near-stationary target. The weapons can be divided into two broad categories: Go-onto-target (GOT) and go-onto-location-in-space (GOLIS) guidance systems. Guidance systems are divided into different categories according to whether they are designed to attack fixed or moving targets. ballistic missile with a highly accurate inertial guidance system was the short-range Redstone. Skinner's attempt to develop a pigeon-guided missile. Project Pigeon was American behaviorist B.F. In World War II, guided missiles were first developed, as part of the German V-weapons program. The concept of missile guidance originated at least as early as World War I, with the idea of remotely guiding an airplane bomb onto a target. 3.1.3 Line-of-sight beam riding guidance.3.1.1.4 Automatic command to line-of-sight.3.1.1.3 Semi-automatic command to line-of-sight.3.1.1.2 Semi-manual command to line-of-sight.3.1.1.1 Manual command to line-of-sight.

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