Does AAA support the design of vectored thrust aircraft?

Vectored thrust can be accounted for in AAA by using different flight conditions. The engine inclination angle can be changed from flight condition independent to dependent. Then in different flight conditions the engine inclination angle can be set to a different value. So the answer is yes. The weight methods of the systems do not account for a gear box or a motor to change the engine inclination, so that will need to be added in as a used defined weight, which is possible in Class II weights.