Estimation of stability and control derivatives, Static lateral-directional stability and trim

Estimation of aircraft dynamical characteristics, handling qualities

Performance analysis: Steady level flight, Minimum thrust required for level flight, range and loiter endurance

Steady climbing and descending flight, Best angle and rate of climb

Time to climb and fuel to climb, Level turning flight, instantaneous turn rate, sustained turn rate

Energy maneuverability methods of optimal climb trajectories and turns