TY  - RPRT
TI  - Multi-Stage Stabilized Continuation for Indirect Optimal Control of Hypersonic Trajectories.
AU  - Vedantam, Mihir
AU  - Akella, Maruthi
AU  - Grant, Michael James
PY  - 2020
DO  - 10.2514/6.2020-0472
UR  - https://www.osti.gov/biblio/1761050
ID  - 1761050
ER  -