The concept of aeroassisting for orbital transfer has been recognised as one of the critical technologies for pioneering the space frontier. In space transportation systems, aeroassisting (or aerobraking), defined as the deceleration resulting from the effects of atmospheric drag upon a vehicle during orbital operations, opens new mission opportunities, especially with regard to the establishment of the permanent Space Station Freedom and space explorations to other planets such as Mars. The main areas of research reported in this monograph are atmospheric entry problems by the method of matched asymptotic expansions, coplanar and non-coplanar orbital transfers with aeroassist technology, orbital plan change with aerocruise, and neighbouring optimal guidance. A special feature is the bibliography which will provide the reader with a literature status for further research.
Atmospheric Entry.- Full Optimal Control for Coplanar Orbital Transfer.- Fuel Optimal Control for Non-Coplanar Orbital Transfer.- Orbital Plane Change with Aerocruise.- Deterministic Optimal Guidance for Orbital Transfer.- Bibliography.
Series: CSCW: Computer Supported Cooperative Work
Number Of Pages: 182
Publisher: Springer-Verlag Berlin and Heidelberg Gmbh & Co. Kg
Country of Publication: GB
Dimensions (cm): 23.39 x 15.6
Weight (kg): 0.29