Attainability Analysis for Entry Vehicles Based on Differential Evolution

Table 1

Constraints of the trajectories according to the landing footprint.

	max(𝑄̇)	max(𝑞)	max(𝑛)	|Δ𝑟(𝑡𝑓)|	|Δ𝑣(𝑡𝑓)|	|Δ𝛾(𝑡𝑓)|
	(W/m^2)	(N/m^2)	(g)	(m)	(m/s)	(degree)
Maximum	431249	9916	2.41	1952	19.7	0.96
Mean	406557	8614	1.83	955	9.6	0.44
Minimum	346819	7242	1.56	5	0.8	0.01
Standard	26432	584	0.13	442	5.9	0.28