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== Approach == | == Approach == | ||
{{FGCquote | |||
|1= you will obtain the "maximal theoretical performance" of each system (in isolation), so that you can check if/how complexity of the 3D model and/or FDM is playing a role here. | |||
Next, you would do the same thing with Nasal code, i.e. by disabling it entirely and watching performance then. | |||
|2= {{cite web | |||
| url = http://forum.flightgear.org/viewtopic.php?p=264313#p264313 | |||
| title = <nowiki>Re: Su-15</nowiki> | |||
| author = <nowiki>Hooray</nowiki> | |||
| date = Nov 13th, 2015 | |||
}} | |||
}} | |||
We will be testing different components, and features, of each aircraft in isolation, to exclude certain factors and determine if/how performance is affected by certain features. | We will be testing different components, and features, of each aircraft in isolation, to exclude certain factors and determine if/how performance is affected by certain features. | ||