Method for identifying maneuvering state of hypersonic aircraft
A hypersonic and state recognition technology, applied in neural learning methods, character and pattern recognition, instruments, etc., can solve problems such as difficult feature extraction, fast flight speed, and wide space range
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Embodiment 1
[0077] like figure 1 As mentioned above, this embodiment provides a recognition process of a method for recognizing the maneuvering state of a hypersonic aircraft, and the specific processing process of the recognition method is as follows:
[0078] Step 1: Maneuver modeling of hypersonic vehicle;
[0079] Step 2: Divide the maneuvering categories of the hypersonic aircraft, construct a feature parameter set, and screen the feature parameters through information gain and information gain rate, and use the different controls obtained by the hypersonic aircraft maneuvering modeling in step 1 under different initial variable conditions. A parameter model, generating a trajectory library containing the maneuvering trajectories of the hypersonic aircraft in different maneuvering states, and using the feature identification parameter information contained in the trajectory library as training data;
[0080] Step 3: establish a hypersonic aircraft maneuvering state recognition model...
Embodiment 2
[0189] In this embodiment, the above method is verified in combination with a specific calculation example, and the process is as follows:
[0190] Firstly, it is verified on the typical hypersonic vehicle trajectory, and two aircraft maneuvering trajectories are designed. Among them, the maneuvering state of trajectory 1 is the right turn of balance gliding, and the maneuvering state of trajectory 2 is jumping and gliding without maneuvering, such as image 3 shown. The parameters of the radar are set as follows: the distance error is 200m, the azimuth error is 0.1°, the pitch angle error is 0.1°, and the sampling rate is 0.5s.
[0191] Then, it is verified on the multi-sample aircraft trajectory, and 24 hypersonic aircraft trajectories (three for each maneuvering state) observed in real time by radar are selected, with a total of 43,200 trajectory points.
[0192] The method described in step 4 converts the state information of the hypersonic aircraft observed by the radar...
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