Zobrazeno 1 - 9
of 9
pro vyhledávání: '"H. J. Kelley"'
Publikováno v:
Automatica. 7:37-43
The accelerated gradient projection technique is a terminally quadratically-convergent parameter optimization algorithm for use with non-linear constraints. This algorithm is used to find the minimum-propellant ascent trajectory of a multi-stage rock
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7d58200428d7d55e919edbadf32eba18
https://doi.org/10.1016/0005-1098(71)90077-x
https://doi.org/10.1016/0005-1098(71)90077-x
Publikováno v:
AIAA Journal. 7:879-884
Multistage rocket trajectories optimized by second order numerical technique and digital computer program, considering coasting, vacuum flight and transition times
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d7e909a600044808c321e45a74e479d0
https://doi.org/10.2514/3.5239
https://doi.org/10.2514/3.5239
Autor:
T. N. Edelbaum, H. J. Kelley
Publikováno v:
Journal of Aircraft. 7:93-95
Asymptotic expansions and energy methods applied to three dimensional aircraft maneuvers involving energy climbs and turns
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c4326d98161306d284bab887cf731884
https://doi.org/10.2514/3.44130
https://doi.org/10.2514/3.44130
Publikováno v:
AIAA Journal. 8:2091-2093
Conjugate direction minimization procedure based on sequences and inferred second partial derivative matrix inverse
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::29112f2f67b355ec4eb2158772ecee39
https://doi.org/10.2514/3.6063
https://doi.org/10.2514/3.6063
This paper conducts a comparative study of periodic and steady-state solutions for aircraft cruise-dash optimization. The solutions are in the point- mass model. The cost functional is an average weighted sum of the fuel used and the time taken. Prev
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0826a0720d284415020f65826d88929d
https://doi.org/10.21236/ada207855
https://doi.org/10.21236/ada207855
This 15 month effort developed an orbital maneuver sequence optimization computer program and applied it to the generation of optimal co orbital attack maneuver sequences and to the generation of optimal evasion and return maneuver sequences. Rocket
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c222ab8d3bd9fa8a90ff8861bdc7fc0e
https://doi.org/10.21236/ada165138
https://doi.org/10.21236/ada165138
Autor:
L. Lefton, H. J. Kelley
Publikováno v:
15th Aerospace Sciences Meeting.
A chase in a horizontal plane between a pursuer with a large capture radius and a more maneuverable evading vehicle is examined with constant-speed vehicle models. An approximation to the 'sidestepping' maneuver of the Homicidal Chauffeur Game is mod
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6c2dffa88c59bc32087ba36926f6db05
https://doi.org/10.2514/6.1977-35
https://doi.org/10.2514/6.1977-35
Autor:
H. J . Kelley
Publikováno v:
Journal of Aircraft. 14:512-512
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::757ce605ec376baf63247b3d813848c4
https://doi.org/10.2514/3.58811
https://doi.org/10.2514/3.58811
Autor:
Walter F. Denham, H. J. Kelley
Publikováno v:
Journal of Optimization Theory and Applications. 4:72-72
Sequential vector estimation of matrix of second partial derivatives, suggesting alternative least squares method
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4a795a2990eeb83a9360d010ced866f2
https://doi.org/10.1007/bf00928718
https://doi.org/10.1007/bf00928718