A Multiconstrained Ascent Guidance Method for Solid Rocket-Powered Launch Vehicles

Table 6

Monte Carlo simulations statistic results.

Terminal state deviation	Maximum/minimum	Mean	Standard deviation
(°)	0.1127	0.0212	0.0268
(m)	3.1650	0.4775	0.4546
(m/s)			12.7036
(°)			0.7303
(s)			1.0756