Mechanism and Kinematics for Flapping Wing Micro Air Vehicles Maneuvering Based on Bilateral Wings

Table 2

Maximums, minimums, means, and amplitudes of and .

	τ	(°)	(°)	(°)	(°)		(°)	(°)	(°)	(°)
DCRM	0.0	41.57	−28.27	6.65	34.92	0	41.57	−28.27	6.65	34.92	0
	0.1	41.40	−28.16	6.62	34.78	−0.40%	41.50	−28.56	6.52	35.08	0.46%
	0.2	41.09	−28.26	6.41	34.68	−0.69%	41.46	−29.05	6.21	35.25	0.95%
	0.3	40.65	−28.58	6.04	34.62	−0.86%	41.16	−29.71	5.73	35.43	1.46%
	0.4	40.09	−29.14	5.48	34.62	−0.86%	40.67	−30.54	5.07	35.61	1.98%
	0.5	39.42	−29.97	4.72	34.70	−0.63%	39.99	−31.53	4.23	35.77	2.43%
SCSM	0.0	45.00	−28.29	8.35	36.65	0	45.00	−28.29	8.35	36.65	0
	0.1	47.29	−30.25	8.52	38.77	5.78%	42.88	−26.56	8.16	34.72	−5.27%
	0.2	49.76	−32.46	8.65	41.11	12.78%	40.91	−25.01	7.95	32.96	−10.07%
	0.3	52.43	−34.99	8.72	43.71	19.26%	39.09	−23.62	7.73	31.36	−14.43%
	0.4	55.30	−37.87	8.72	46.59	27.12%	37.40	−22.38	7.51	29.89	−18.44%
	0.5	58.39	−41.18	8.61	49.79	35.85%	35.84	−21.25	7.30	28.54	−22.13%