A Guidance Law Identification and Filtering Method for Proportional Guidance
A technology of proportional guidance and guidance law, applied in non-electric variable control, control/regulation system, three-dimensional position/course control, etc., can solve problems such as low estimation accuracy and inaccurate MMAE filter model, and achieve improved estimation accuracy Effect
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specific Embodiment approach 1
[0032] Specific implementation mode 1: A proportional guidance guidance law identification and filtering method in this implementation mode is specifically prepared according to the following steps:
[0033] Step 1: The pursuer has two motion models: the saturated motion model when the controller is saturated and the PN guidance law motion model when the controller is not saturated; establish the state equation of the PN guidance law motion model in the pitch plane, and the PN guidance law motion model in the The state equation of the yaw plane, the state equation of the controller saturation motion model in the pitch plane, and the state equation of the controller saturation motion model in the yaw plane; evader is a ballistic missile; pursuer is an intercept missile; PN guidance law is proportional guidance guidance law;
[0034] Step 2: According to the state equation of the PN guidance law motion model in the pitch plane in step 1, the state equation of the PN guidance law...
specific Embodiment approach 2
[0038] Embodiment 2: The difference between this embodiment and Embodiment 1 is that the pursuer in the step 1 has two motion models: a saturated motion model when the controller is saturated and a PN guidance law motion model when the controller is not saturated; Establish the state equation of the PN guidance law motion model in the pitch plane, the state equation of the PN guidance law motion model in the yaw plane, the state equation of the controller saturation motion model in the pitch plane, and the state equation of the controller saturation motion model in the yaw plane ; The specific process is:
[0039] In the missile penetration scenario, if the penetrating ballistic missile wants to evade the interception of the intercepting missile launched by the opponent’s missile defense system, it is the evader, called evader, and all physical quantities related to it contain the subscript e; the intercepting missile is the hunting party , called the pursuer, and all physical...
specific Embodiment approach 3
[0058] Specific embodiment three: the difference between this embodiment and specific embodiment one or two is: in described step 2, according to the state equation of the PN guidance law motion model of step one in the pitch plane, the PN guidance law motion model in the yaw plane The state equation, the state equation of the controller saturation motion model in the pitch plane and the state equation of the controller saturation motion model in the yaw plane, calculate the state transition matrix of the PN guidance law motion model in the pitch plane, and the PN guidance law motion model in the yaw plane The state transition matrix of the plane, the state transition matrix of the controller saturation motion model in the pitch plane, and the state transition matrix of the controller saturation motion model in the yaw plane; the specific process is:
[0059] The state transition matrix of the PN guidance law motion model in the pitch plane is
[0060]
[0061]
[0062] ...
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