Nonlinear Missile Autopilot Design Based on Angle of Attack Normal Form - Archive ouverte HAL Access content directly
Journal Articles European Journal of Control Year : 2000

Nonlinear Missile Autopilot Design Based on Angle of Attack Normal Form

Emmanuel Devaud
  • Function : Author
Not file

Dates and versions

hal-03896142 , version 1 (13-12-2022)

Identifiers

  • HAL Id : hal-03896142 , version 1

Cite

Houria Siguerdidjane, Emmanuel Devaud. Nonlinear Missile Autopilot Design Based on Angle of Attack Normal Form. European Journal of Control, 2000. ⟨hal-03896142⟩
14 View
0 Download

Share

Gmail Facebook Twitter LinkedIn More