A Linear Parameter Varying Controller for a Re-entry Vehicle Benchmark

Author:

Marcos Andrés,Bennani Samir

Publisher

Springer Berlin Heidelberg

Reference19 articles.

1. Balas, G.J.: Flight control law design: An industry perspective. In: European Control Conference, Cambridge, UK (September 2003)

2. Jackson, E.B., Cruz, C.I., Ragsdale, W.A.: Real-Time Simulation Model of the HL-20 Lifting Body. NASA Technical Memorandum 107580 (July 1992)

3. Jackson, E.B., Cruz, C.I.: Preliminary Subsonic Aerodynamic Model for Simulation Studies of the HL-20 Lifting Body. NASA Technical Memorandum 4302 (1992)

4. Cruz, C.I., Ware, G.M.: Control Effectiveness and Tip-Fin Dihedral Effects for the HL-20 Lifting-Body Configuration at Mach Numbers from 1.6 to 4.5. NASA Technical Memorandum 4697 (1995)

5. Scallion, W.I.: Aerodynamic Characteristics and Control Effectiveness of the HL-20 Lifting Body Configuration at Mach 10 in Air. NASA Technical Memorandum 209357 (September 1999)

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