Control Allocation Design of Reaction Control System for Reusable Launch Vehicle

Table 1

Control moments of thrusters.

No.	Roll moment (kN*m)	Yaw moment (kN*m)	Pitch moment (kN*m)
1	−0.82	0	+14.22
2	+0.82	0	+14.22
3	+0.17	+14.22	0
4	−0.17	−14.22	0
5	+0.17	+13.77	0
6	−0.17	−13.77	0
7	+0.17	+13.31	0
8	−0.17	−13.31	0
9	−1.42	+10.06	+10.06
10	+1.42	−10.06	+10.06
11	+0.59	+10.06	−10.06
12	−0.59	−10.06	−10.06