Optimal Powered Aerogravity-Assist Trajectories

[1]  Fayyaz A. Lohar,et al.  Optimal atmospheric trajectory for aerogravity assist with heat constraint , 1995 .

[2]  Peter J. Edelman,et al.  Design and Optimization of Interplanetary Aerogravity-Assist Tours , 2014 .

[3]  A. Prado,et al.  Powered aero-gravity-assist maneuvers considering lift and drag around the Earth , 2017 .

[4]  Michèle Lavagna,et al.  Interplanetary mission design with aero-assisted manoeuvres multi-objective evolutive optimization , 2005 .

[5]  Fayyaz A. Lohar,et al.  Optimal atmospheric trajectory for aero-gravity assist , 1994 .

[6]  James M. Longuski,et al.  DESIGN OF AEROGRAVITY-ASSIST TRAJECTORIES , 2000 .

[7]  Antonio M Mazzaracchio.  Flight-Path Angle Guidance for Aerogravity-Assist Maneuvers on Hyperbolic Trajectories , 2015 .

[8]  K. Havey.  Entry Vehicle Performance in Low-Heat-Load Trajectories , 1982 .

[9]  D. D. Mueller,et al.  Fundamentals of Astrodynamics , 1971 .

[10]  James E. Randolph,et al.  Hypersonic Maneuvering for Augmenting Planetary Gravity Assist , 1992 .

[11]  Peter J. Edelman,et al.  Optimal Aerogravity-Assist Trajectories Minimizing Total Heat Load , 2017 .

[12]  A. D. Ruiter,et al.  Powered swing-by in the elliptic restricted three-body problem , 2018, Monthly Notices of the Royal Astronomical Society.

[13]  James E. Randolph,et al.  Solar system 'fast mission' trajectories using aerogravity assist , 1992 .

[14]  Anil V. Rao,et al.  Algorithm 902: GPOPS, A MATLAB software for solving multiple-phase optimal control problems using the gauss pseudospectral method , 2010, TOMS.

[15]  T. R. F. Nonweiler,et al.  Aerodynamic Problems of Manned Space Vehicles , 1959, The Journal of the Royal Aeronautical Society.

[16]  Yi Qi,et al.  Mechanical analysis of lunar gravity assist in the Earth–Moon system , 2015 .

[17]  M. E. Tauber,et al.  Stagnation-point radiative heating relations for earth and Mars entries , 1991 .

[18]  Angelo Miele,et al.  Gamma guidance of trajectories for coplanar, aeroassisted orbital transfer , 1990 .

[19]  Radhakant Padhi,et al.  Correction: Angle-Constrained Terminal Guidance Using Quasi-Spectral Model Predictive Static Programming , 2020 .

[20]  H. London,et al.  Change of Satellite Orbit Plane by Aerodynamic Maneuvering , 1962 .

[21]  A. Prado,et al.  Application of Impulsive Aero-Gravity Assisted Maneuvers in Venus and Mars to Change the Orbital Inclination of a Spacecraft , 2019, The Journal of the Astronautical Sciences.

[22]  Lorenzo Casalino,et al.  Simple Strategy for Powered Swingby , 1997 .

[23]  Alessandra F. S. Ferreira,et al.  Analytical study of the swing-by maneuver in an elliptical system , 2018, Astrophysics and Space Science.