Applied LPV Control with Full Block Multipliers and Regional Pole Placement

Table 1

Vehicle's details.

Name	Symbol	Value
Initial/final Mass	𝑚0/𝑚𝑓	500/250 kg
Initial/final Inertia	𝐽𝑥0/𝐽𝑥𝑓	60/30 kg m^2
Initial/final Inertia	𝐽𝑡0/𝐽𝑡𝑓	200/100 kg m^2
Aerodynamic Derivative	𝐷𝛼=𝜕𝐹^𝑧𝑎𝜕𝑞2	0.1963
Nominal thrust	𝑓𝑛	20×10^3 N
Distance from CM to nozzle	ℓ	2 m
Distance from CM to CP	ℓ1	1 m
Maximum Dynamic Pressure	𝑄0max	3×10^5N/m^2