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Static interpolated ℋ∞ loop-shaping controllers for missile autopilot synthesis., and . CDC, page 2385-2392. IEEE, (2007)Gain-Scheduled Autopilot Design with Anti-Windup Compensator for a Dual-Spin Canard-Guided Projectile., , , , and . CCTA, page 156-161. IEEE, (2020)Hardware-in-the-loop experimental setup development for a guided projectile in a wind tunnel., , , , and . AIM, page 458-463. IEEE, (2014)Robust Design for Highly Agile Missile Autopilots., , and . MED, page 67-72. IEEE, (2020)Flight Dynamics Modeling of Dual-Spin Guided Projectiles., , , , and . IEEE Trans. Aerosp. Electron. Syst., 53 (4): 1625-1641 (2017)Fixed structure ℋ∞ Control for a canard-guided projectile pitch/yaw dynamics autopilot design., , , , and . ECC, page 594-599. IEEE, (2014)Autopilot Design for Dual-Spin Projectiles using Incremental Nonlinear Dynamic Inversion., , , and . MED, page 444-449. IEEE, (2022)Sensor position influence on modeling and control of 155mm canard-guided spin-stabilized projectiles., , , , and . CoDIT, page 358-363. IEEE, (2014)Modelling and stability analysis of the 155 mm spin-stabilised projectile equipped with steering fins., , and . Int. J. Model. Identif. Control., 14 (3): 189-204 (2011)Robust gain scheduled control of a space launcher by introducing LQG/LTR ideas in the NCF robust stabilisation problem., , , and . CDC, page 2393-2398. IEEE, (2007)