1. Structured singular-value analysis of the vega launcher in atmospheric flight;Simplício;J. Guid. Control Dyn.,2016
2. Theory of Artificial Stabilization of Missiles and Space Vehicles with Exposition of Four Control Principles;Hoelker,1961
3. J. Livingston, J. Redus, Load-reducing flight control systems for the Saturn V with various payloads, in: The 1968 AIAA Control and Flight Dynamics Conference, Pasadena, CA, 1968.
4. Guidance, Steering, Load Relief and Control of an Asymmetric Launch Vehicle;Boelitz,1989
5. Model Predictive Control for Ascent Load Management of a Reusable Launch Vehicle;Martin,2002