Method and system for semi-physical simulation test of visual unmanned aerial vehicle flight control
A semi-physical simulation and flight control technology, applied in general control systems, control/adjustment systems, instruments, etc., can solve the problem of not being able to display flight status and data in real time and intuitively
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[0071] First, in terms of initial settings: the initial heading is 0 (true north);
[0072] After starting the real-time code and establishing the communication between the host machine and the target machine, it is necessary to convert the Simulink model into real-time embedded code and download it to the xPC target machine. At this time, it is necessary to configure the simulation parameters and the RTW generated file type. When setting the simulation parameters and the RTW generated file type, select the Real-Time Workshop / Target Selection dialog box in the model window menu, set the System target file to xpctarget.tlc, and set the languages to C.
[0073] In terms of RTW parameter setting: only a few parameters need to be modified during testing:
[0074] (1) Solver (solver) uses ode4Runge-Kutta (fourth-order Runge-Kutta method). The calculation error of the fourth-order Runge-Kutta method is small, and it can realize self-starting. When the model is not very complicate...
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