Research Article

Applied LPV Control with Full Block Multipliers and Regional Pole Placement

Table 1

Vehicle's details.

Name Symbol Value

Initial/final Mass 𝑚 0 / 𝑚 𝑓 5 0 0 / 2 5 0  kg
Initial/final Inertia 𝐽 𝑥 0 / 𝐽 𝑥 𝑓 6 0 / 3 0  kg m2
Initial/final Inertia 𝐽 𝑡 0 / 𝐽 𝑡 𝑓 2 0 0 / 1 0 0  kg m2
Aerodynamic Derivative 𝐷 𝛼 = 𝜕 𝐹 𝑧 ğ‘Ž 𝜕 ğ‘ž 2 0 . 1 9 6 3
Nominal thrust 𝑓 𝑛 2 0 × 1 0 3  N
Distance from CM to nozzle ℓ 2  m
Distance from CM to CP ℓ 1 1  m
Maximum Dynamic Pressure 𝑄 0 m a x 3 × 1 0 5 N / m 2