1. The actuators subsystem currently consists of first order actuator transfer functions and limiters that bound the permissible range of symmetric δsymand antisymmetric δasycontrol surface deflections (-25 degrees and -20 degrees, respectively) and commanded motor voltage (0 - 20 volts). The sensor subsystem currentlycontains no dynamics but will permit sensor modelstobeaddedatalatertime.
2. The longitudinal and lateral-directional subsystems consist of additional subsystems that systematically build up the equations of motion as derived in reference6. The equations representthe six degree-offreedommotion of a rigid aircraft relative to a flat, non-rotating earth. The atmosphere is representedusing the 1976 StandardAtmospheremodel.[6]UFMAV AeroModel
3. The functions are in the form of Taylor series;Theaerodynamicmodelwasobtainedprimarilyfrom NASA
4. Experimental Trim 1.0 18,900 10.4 -6.5 1.6 20,600 5.4 -3.5 2.0 21,900 4.0 -2.5
5. Analytical Trim (Simplified) 1.0 - 11.2 -5.6 1.6 - 5.4 -2.5 2.0 - 3.5 -1.9