Ascent, transition, entry, and abort guidance algorithm design for the X-33 vehicle
- 10 August 1998
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Entry Guidance and Trajectory Control for Reusable Launch VehicleJournal of Guidance, Control, and Dynamics, 1997
- Shuttle entry guidance revisited using nonlinear geometric methodsJournal of Guidance, Control, and Dynamics, 1994