6Cloutier James R, Zipfel Peter H. Hypersonic guidance via the state-dependent ricotta equation control method. International Conference on Control Application, USA, 1999.
7Overview of Hypersonic in Europe. 17th AIAA Interna- tional Space Planes and Hypersonic Systems and Tech- nology Conference. 2012.
2Rasmussen M L. Waverider configurations derived from inclined circular and elliptic cones[J]. Journal of Spacecraft and Rockets, 1980,17(6):537- 545.
3Corda S. Viscous optimized hypersonic waveriders designed from flows over cones and minimum drag bodies [D]. Maryland:University of Maryland College Park, 1988.
4Bowcutt K G. Optimization of hypersonic waveriders derived from cone flows-inluding viscous effects [D]. Maryland: University of Maryland College Park, 1986.
5Lobbia M, Suzuki K. Design and analysis of payload-optimized waveriders [R].AIAA2001-1849.
6Eckert E R G. Engineering relations for heat transferred friction in high velocity laminar and turbulent boundary layer flow over surface with constant pressure and temperature[J]. Transaction of the ASME, 1970, 78 (5):855.
7Bowcutt K G, Anderson J D. Viscous optimized waverider designed from ax symmetric flow fields [R].AIAA 88-20369.
8Vanmol D O. Heat transfer characteristics of hypersonic waverider with an emphasis on the leading edge effects[D]. Maryland:University of Maryland College Park, 1990.
9Deb K, Pratap A, Agrawal S, et al. A fast and elitist multi-objective genetic algorithm: NSGA-II [R]. KanGAL Report No. 200001.
