Method for determining multi-state tracking guidance parameters
A guidance parameter, multi-state technology, applied in attitude control, non-electric variable control, altitude or depth control, etc., can solve problems such as inability to achieve decoupling control
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[0045] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below with reference to the accompanying drawings and examples.
[0046] This embodiment provides a method for determining multi-state tracking and guidance parameters, which is suitable for the guidance process of the gliding aircraft in the balanced gliding segment, thereby solving the design and coordination problems of multi-state tracking and guidance parameters, and providing guidance for the design of guidance parameters and gliding guidance. The realization provides design basis and support.
[0047] figure 1 It is a schematic flowchart of a method for determining multi-state tracking and guidance parameters in an embodiment of the present invention. Such as figure 1 As shown, the method for determining multi-state tracking guidance parameters in the embodiment of the present invention includes: .
[0048] ...
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