Based on some actual high altitude range in hypersonic flight test,the characters of wind such as mean wind,gust,turbulence and random wind are analyzed,and then the mathematic models of ground wind,low/middle-altitude and high-altitude have been established.

Overall plan for hypersonic boost-flight experiment technology is investigated in detail for the free-flight test of hypersonic vehicle under nominal design conditions.

Optimization of glide trajectory for a hypersonic vehicle;

Heat flux measurement test of the hypersonic vehicle;

Fuzzy adaptive control for hypersonic vehicle via Backstepping method;

Eigenvalue perturbation analysis of thrust law effects on hypersonic flight dynamics;

Currently,hypersonic flight has been a widely attention-getting technology for the requirement generated by the space exploitation and the new military strategy.