Sliding Mode Observer and Control Design with Adaptive Parameter Estimation for a Supersonic Flight Vehicle

Table 2

Flight Vehicle Constants.

Symbol	Quantity
𝐼𝑦	247.43662 kg m^2
𝑑	0.2286 m
𝑆	0.0409 m^2
𝑚	204.108 kg
𝜏𝑎	1/150 s
𝑔	9.81 m/s^2