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

Table 1

Aerodynamic Polynomial Coefficients.

𝛽1𝑛=19.3734	𝛽1𝑚=40.4396
𝛽2𝑛=31.0225	𝛽2𝑚=−64.0147
𝛽3𝑛=−9.717	𝛽3𝑚=2.9221
𝑑𝑛=−1.9481	𝑑𝑚=−11.8029