Model-Based Design, HIL Testing, and Rapid Control Prototyping of a Low-Cost POC Quadcopter with Stability Analysis and Control

Table 7

Summarized system.

Sr. no.	Parameter	Value	Value (weight)	Unit
1	Required RPM FT	8281	10985	RPM
2	Required kv FT	753	990	Kv
3	Required nom. kV FT	904	1188	Kv
4	Pout FT	136	318	W
5	Pin FT	163.2	380	RPM
6	Motor ampere	15	35	A
7	Required ESC	18	42	A
8	Battery rating	14	32.3	C
9	Endurance FT	4.16	1.78	Minutes
10	Required RPM H	5233	6947	RPM
11	Pout H	34.4	80.4	W
12	Pin H	41.28	96.4	W
13	Endurance H	15.6	9	Minutes
14	Flight time (average)	9.88	4.35	Minutes