Author name: Akash Babu S L

The pitch rate is the rate at which an aircraft rotates about its lateral axis.   q: Pitch rate Melevator​: Elevator control effectiveness c: Mean aerodynamic chord of the wing Ipitch​: Moment of inertia about the pitch axis

The roll rate is the rate at which an aircraft rotates about its longitudinal axis   p: Roll rate L aileron​: Aileron control effectiveness (force generated by the ailerons) b: Wingspan of the aircraft Iroll​: Moment of inertia about the roll axis

Parasite drag is a type of drag that is not associated with the production of lift. It includes form drag, skin friction drag, and interference drag   D0​ :Parasite Drag q :Dynamic Pressure S :Wing Reference Area CD0​​ :Zero-lift Drag Coefficient

The Airspeed-Altitude Correction Factor (Fcor​) is an adjustment factor used to correct indicated airspeed for changes in altitude   h represents the altitude above sea level.

Dutch Roll Mode is a dimensionless parameter that represents the ratio of the change in yaw rate (δr) to the change in aileron deflection (δa). δr represents the change in yaw rate δa represents the change in aileron deflection

The Airspeed-Altitude Correction Factor is used to correct the true airspeed (TASactual​) for non-standard atmospheric conditions   TASstandard​ represents the true airspeed under standard atmospheric conditions. TASactual​ represents the true airspeed at the actual altitude.

Zero Fuel Weight is the weight of an aircraft excluding the weight of its fuel   WZF​ is the Zero Fuel Weight. WTO​ is the Takeoff Weight Fuel Weight is the weight of the fuel on board

Mach Trim is the change in the pitching moment coefficient required to trim an aircraft at a specific Mach number.   CLtrim: trim lift coefficient 

The Ground Roll Distance (GRD) is the distance traveled by an aircraft on the ground from lift-off until it becomes airborne.   GRD:Lift-off Speed Vlof : Lift-off Speed g: Acceleration Due to Gravity μ:  Coefficient of Friction

The Sonic Boom Overpressure is used to estimate the overpressure generated by a sonic boom produced by an aircraft traveling at supersonic speeds ΔP is the sonic boom overpressure, ρ is the air density, Vboom​ is the velocity of the aircraft producing the sonic boom, γ is the specific heat ratio.