Evaluation system for semi-physical simulation test under non-reference condition
A semi-physical simulation and evaluation system technology, applied in design optimization/simulation, special data processing applications, geometric CAD, etc., can solve the problems of inability to accurately evaluate the effect of semi-physical simulation test
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Embodiment 1
[0102] A specific embodiment of the present invention discloses a kind of evaluation system of semi-physical simulation test under no benchmark condition, such as figure 1 As shown, it includes a simulation data acquisition module, a single-variable uncertainty calculation module, a comprehensive uncertainty calculation module, and an evaluation result judgment module connected in sequence.
[0103] The simulation data acquisition module is used to receive the simulation data of all uncertainty output variables in multiple semi-physical simulation tests under the same test condition, and send them to the single variable uncertainty calculation module.
[0104] The univariate uncertainty calculation module is used to construct the data distribution probability envelope of each uncertainty output variable based on the obtained simulation data, and then determine the random uncertainty and probability variance of each uncertainty output variable. The degree of certainty is sent t...
Embodiment 2
[0110] The optimization is carried out on the basis of Example 1, and the hardware-in-the-loop simulation test is an aircraft hardware-in-the-loop simulation test. The evaluation system is used for aircraft hardware-in-the-loop simulation tests, or other types of hardware-in-the-loop simulation tests.
[0111] For the hardware-in-the-loop simulation test of the aircraft, the uncertainty output variables include at least one of landing point deviation, attitude, angle of attack and sideslip angle, position, velocity, and the like.
[0112] Specifically, the landing point deviation is the deviation between the landing point position of the aircraft obtained from the hardware-in-the-loop simulation test and the target position. Aircraft attitude includes pitch angle, yaw angle, roll angle, etc.; aircraft position includes altitude, lateral, and longitudinal positions. For simplicity of calculation, the attitude and position of the aircraft at the landing point of each hardware-i...
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