Optimal ascent guidance for a hypersonic vehicle

1996 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1996, Pages 1-10

  Paus, Michael ^a,b   Well, Klaus H ^a  

^a UNIVERSITY OF STUTTGART   (Germany)

^b NONE   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE VEHICLES; LINEAR CONTROL SYSTEMS; NONLINEAR PROGRAMMING; OPTIMIZATION; PIECEWISE LINEAR TECHNIQUES;

ASCENT GUIDANCES; DYNAMIC INVERSION; INTEGRATION METHOD; MODEL REDUCTION; PIECEWISE-LINEAR CONTROLS; REAL TIME CAPABILITY; TRAJECTORY OPTIMIZATION; TWO STAGE TO ORBITS;

AIR NAVIGATION;

EID: 84959148715     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. Schultz, R. U, Hoffmann, M. J., Case, A. M, Sheikh, S. I., Navigation, Guidance, and Trajectory Optimization for Hypersonic Vehicles.
2. Corban, J.E., Calise, A.J., Flandro, G.A. Rapid Near- Optimal Aerospace Plane Trajectory Generation and Guidance, Joiumal of Guidance, Navigation, and Control, Vol. 14, No. 6, Nov-Dec. 1991, pp. 1181-1190.
3. Mease, K.D., Buren, M.A. Geometric Synthesis of Aerospace Plane Ascent Guidance Logic, Automatica, Vol. 30, No.12,pp. 1839-1849,1994.
4. Hermann, J.A., and Schmidt O.K. SSTO Mission Analysis of a Generic Airbreathing Hypersonic Vehicle, AIAA Guidance, Navigation, and Control Conference, Baltimore, USA, 1995.
5. Paus, M. A General Approach to Optimal Real-Tirae Guidance of Dynamic Systems Based on Nonlinear Programming, AIAA Conference on Guidance, Navigation and Control, Hilton Head, USA, 1992.
6. Paus, M. A General Numerical Method for Optimal Guidance of Dynamic Systems, Ph.D Thesis, University of Stuttgart, 1996.
7. Paus, M., Grimm, W, and Well, K.H. Real-Time Optimization for the Guidance if Dynamic Systems, Proceedings of the ECMI 94 (European Consortium of Mathematics in Industry), Kaiserslautem Germany, September 1994.
8. Stoer, J., Bulirsch, R., Introduction into Numerical Analysis, Springer, New York, Heidelberg, Berlin, 1980.
9. Miele, A. Flight Mechanics - Theory of Flight Path, Addison-Wesley, Reading, Massachusets, 1962.
10. Koelle, D.E. Sanger 2 Aerodynamic and Propulsive Data, Private Communication, 1989.
11. Jansch, C., Schnepper K., Well K.H.Multiphase trajectory optimization methods with applications to hypersonic vehicles. In: Applied mathematics in aerospace science and engineering (Miele and Salvetti, Eds.), chapter 8, Plenum Press, New York, 1994.