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Sensor position influence on modeling and control of 155mm canard-guided spin-stabilized projectiles.

, , , , and . CoDIT, page 358-363. IEEE, (2014)

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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)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)Controller design point selection for linearized gain scheduling., , , , and . ACC, page 1574-1579. IEEE, (2017)An Interpolated Model Recovery Anti-Windup for a Canard-Guided Projectile Subject to Uncertainties., , , and . ECC, page 1693-1698. IEEE, (2021)Comparison of two H∞ loop-shaping robust autopilot structure configurations for a 155mm spin-stabilized canard-guided projectile., , , , and . MED, page 1147-1152. IEEE, (2014)Fixed structure robust control design for the 155mm canard-guided projectile roll-channel autopilot., , , and . MED, page 155-160. IEEE, (2013)Sensor position influence on modeling and control of 155mm canard-guided spin-stabilized projectiles., , , , and . CoDIT, page 358-363. IEEE, (2014)Optimal control and numerical optimization for missile interception guidance., , , , , and . ECC, page 1249-1255. IEEE, (2014)