Development of Real-Time Maneuver Library Generation Technique for Implementing Tactical Maneuvers of Fixed-Wing Aircraft

Table 4

Boundary conditions for attitude trajectory [18].

(s)	s
(deg)	deg
(deg/s)	deg/s
(deg/s^2)	deg/s^2
(deg/s^3)	deg/s^3
(deg/s^4)	deg/s^4