Man-Machine Modeling and Safety Analysis Method for Landing Process Based on SysML and Simulink

Table 1

Some basic attributes of the system.

No.	Attributes	Symbol	Belonged module	Unit
1	The variation of speed	VT	Equipment	m/s
2	The elevator operating angle		Equipment	rad
3	The variation of attack angle		Equipment	rad
4	The variation of pitch angle		Equipment	rad
5	The variation of pitch angle speed		Equipment	rad/s
6	The variation of aircraft altitude		Equipment	M
7	The mass of aircraft	M	Equipment	Kg
8	Pilot state	E1	Human	-
9	Avionic equipment state	E2	Equipment	-
10	Environmental state	E3	Environment	-