Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77179/1/AIAA-1996-3425-378.pd
The proposed investigation on a Matched Asymptotic Expansion (MAE) method was carried out. It was co...
The problem of determining the trajectories, partially or wholly contained in the atmosphere of a sp...
This note shows that a feasible reference drag profile for the first entry portion of a skip entry c...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76344/1/AIAA-1993-3679-680.pd
With the development of aeroassist technology, either for near-earth orbital transfer with or withou...
The closed-form analytic solution to the equations of motion for ballistic entry developed by Allen ...
Closed-form analytical guidance algorithms are highly desirable in the context of real-time aerospac...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77023/1/AIAA-26742-801.pd
An improved technique for matching the asymptotic solutions of non-linear differential equations is ...
Approximate solutions for flight path angle of reentry vehicle in upper atmospher
The pair of motion equations for entry into a planetary atmosphere is reduced to a single, ordinary,...
This dissertation deals with the development of analytical theories for spacecraft entry into planet...
Approximate optimal atmospheric entry trajectories maximizing terminal function of velocity, heading...
In this paper, an approximate closed-form solution for trajectories of ballistic projectiles is deri...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003.In...
The proposed investigation on a Matched Asymptotic Expansion (MAE) method was carried out. It was co...
The problem of determining the trajectories, partially or wholly contained in the atmosphere of a sp...
This note shows that a feasible reference drag profile for the first entry portion of a skip entry c...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76344/1/AIAA-1993-3679-680.pd
With the development of aeroassist technology, either for near-earth orbital transfer with or withou...
The closed-form analytic solution to the equations of motion for ballistic entry developed by Allen ...
Closed-form analytical guidance algorithms are highly desirable in the context of real-time aerospac...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77023/1/AIAA-26742-801.pd
An improved technique for matching the asymptotic solutions of non-linear differential equations is ...
Approximate solutions for flight path angle of reentry vehicle in upper atmospher
The pair of motion equations for entry into a planetary atmosphere is reduced to a single, ordinary,...
This dissertation deals with the development of analytical theories for spacecraft entry into planet...
Approximate optimal atmospheric entry trajectories maximizing terminal function of velocity, heading...
In this paper, an approximate closed-form solution for trajectories of ballistic projectiles is deri...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003.In...
The proposed investigation on a Matched Asymptotic Expansion (MAE) method was carried out. It was co...
The problem of determining the trajectories, partially or wholly contained in the atmosphere of a sp...
This note shows that a feasible reference drag profile for the first entry portion of a skip entry c...
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