The emergence of current high-interest mission involving aeromaneuvering hypersonic flight has given rise to the corresponding need for preliminary design and performance analyses of such vehicles. This need in turn has motivated efforts to develop simplified analytical and computational methods for parametric analysis of maneuvering hypersonic flight under conditions appropriate to the mission involved. The effort included a review of different formulations of the general equations of motion, their associated coordinate frames, various simplifications of the equations, and previously achieved analytical solutions. This study sought to both extend previous solution methods and to develop new ones. In addition, evaluation of the literature a...
The stability and control of a high-performance aircraft was analyzed, and a design methodology for ...
While continuing the application of the inverse dynamics approach in obtaining the optimal numerical...
AbstractDesign studies are underway for a variety of hypersonic flight vehicles. The National Aero-S...
The effects of aerodynamic forces on trajectories at orbital speeds are discussed in terms of atmosp...
An integrated trajectory/control analysis algorithm has been used to generate trajectories and desir...
Various transition methods are used here to study the viscous effects encountered in low density, hy...
The aero-gravity assist maneuver is here proposed as a tool to improve the efficiency of the gravity...
The classical theory of flight dynamics for airplane longitudinal stability and control analysis was...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76648/1/AIAA-1987-2564-435.pd
The effort was in two areas: (1) development of advanced methods of flight path optimization, and (2...
A maneuver design method that is particularly well-suited for determining the stability and control ...
A tool which generates optimal trajectory/control histories in an integrated manner is generically a...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90726/1/AIAA-2011-6300-100.pd
Computational Fluid Dynamics (CFD) has played a major role in the resurgence of hypersonic flight, o...
This paper summarizes a Langley Research Summer Scholars (LARSS) research project (Summer 1986) deal...
The stability and control of a high-performance aircraft was analyzed, and a design methodology for ...
While continuing the application of the inverse dynamics approach in obtaining the optimal numerical...
AbstractDesign studies are underway for a variety of hypersonic flight vehicles. The National Aero-S...
The effects of aerodynamic forces on trajectories at orbital speeds are discussed in terms of atmosp...
An integrated trajectory/control analysis algorithm has been used to generate trajectories and desir...
Various transition methods are used here to study the viscous effects encountered in low density, hy...
The aero-gravity assist maneuver is here proposed as a tool to improve the efficiency of the gravity...
The classical theory of flight dynamics for airplane longitudinal stability and control analysis was...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76648/1/AIAA-1987-2564-435.pd
The effort was in two areas: (1) development of advanced methods of flight path optimization, and (2...
A maneuver design method that is particularly well-suited for determining the stability and control ...
A tool which generates optimal trajectory/control histories in an integrated manner is generically a...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90726/1/AIAA-2011-6300-100.pd
Computational Fluid Dynamics (CFD) has played a major role in the resurgence of hypersonic flight, o...
This paper summarizes a Langley Research Summer Scholars (LARSS) research project (Summer 1986) deal...
The stability and control of a high-performance aircraft was analyzed, and a design methodology for ...
While continuing the application of the inverse dynamics approach in obtaining the optimal numerical...
AbstractDesign studies are underway for a variety of hypersonic flight vehicles. The National Aero-S...