Reconfigurability Analysis Method for Spacecraft Autonomous Control

Table 3

𝑤_𝑖 matrix.

𝑃	𝑆
	I	II	III	IV
A	1	1/3	1/7	1/13
B	1/2	1/5	1/9	1/16
C	1/4	1/6	1/11	1/18
D	1/8	1/10	1/14	1/19
E	1/12	1/15	1/17	1/20