Attitude Determination Algorithms through Accelerometers, GNSS Sensors, and Gravity Vector Estimator

Table 1

Aerodynamic coefficient interpolation table in function of the Mach number.

M
0.00	0.27	10.74	8.01	19.82	−0.59	50.81	−35.58	−16.65	−225.73	3.02	−0.04	0.00
0.40	0.25	10.88	8.17	19.55	−0.64	53.25	−35.72	−18.09	−232.75	3.29	−0.04	0.42
0.60	0.24	11.10	8.43	19.12	−0.70	57.43	−36.00	−20.39	−245.32	3.57	−0.04	0.43
0.70	0.24	11.24	8.60	18.83	−0.72	60.31	−36.21	−21.82	−254.10	3.71	−0.03	0.44
0.80	0.23	11.40	8.79	18.49	−0.75	63.80	−36.51	−23.39	−264.85	3.84	−0.03	0.44
0.90	0.23	11.45	8.98	17.28	−0.78	67.93	−36.57	−18.48	−276.57	3.98	−0.03	0.45
1.00	0.41	15.12	8.93	44.05	−0.81	71.38	−35.99	15.39	−287.82	4.12	−0.03	0.45
1.10	0.48	15.09	8.99	43.00	−0.83	76.53	−35.54	19.12	−302.58	4.25	−0.03	0.45
1.20	0.46	14.77	8.74	42.60	−0.86	75.29	−35.33	28.92	−304.31	4.39	−0.03	0.44
1.50	0.41	13.99	8.10	41.97	−0.94	86.55	−27.05	26.25	−289.17	4.80	−0.03	0.40
2.00	0.35	13.02	7.28	41.27	−1.07	110.51	−17.62	24.77	−267.48	5.49	−0.02	0.35
2.50	0.30	12.69	6.86	42.25	−1.07	134.47	−13.03	12.50	−255.33	5.49	−0.02	0.30