by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, D.C.?, Springfield, Va.? .
Written in English
|Statement||principal investigator: Ping Lu.|
|Series||NASA contractor report -- NASA CR-192954.|
|Contributions||United States. National Aeronautics and Space Administration.|
|The Physical Object|
Get this from a library! Trajectory optimization for the National AeroSpace Plane: final report, May 1, - [Ping Lu; United States. National Aeronautics and Space Administration.]. Department of Mechanical and Aerospace Engineering School of Engineering and Applied Science Princeton University, Princeton, New Jersey NASA Grant Monitor: D. D. Moerder (NASA-CR) TRAJECTORY OPTIMIZATION AND GIJlDANCE FOR AN AFROSPACE PLANE Final Report, Sept. B - Aug. (Princeton Univ.) 42 p CSCL OIC G3/o5 N Unclas Author: Kenneth D. Mease, Mark A. Vanburen. Trajectory optimization and guidance law development for national aerospace plane applications Article (PDF Available) January with 44 Reads How we measure 'reads'. Trajectory optimization and guidance law development for national aerospace plane applications final report, July 1, to Novem Atlanta, Ga.: [Springfield, Va: School of Aerospace Engineering, Georgia Institute of Technology ; National Technical Information Service, .
In book: (Almost) Impossible Integrals, Sums, and Series, pp Trajectory Optimization and Guidance Law Development for National Aerospace Plane Applications The application of the Author: Erwin Mooij. Mathematical Models for Aircraft Trajectory Design: A Survey 3 lowing accuracy. The last one can be rigorously deﬁned by the mean of trajectory space. The ﬁrst one is a limit case of the second by adding a weight function in the energy functional. Since we may prescribe smoothness accuracy of a simpliﬁedCited by: Part of the Springer Optimization and Its Applications book series (SOIA, volume ) Abstract Over the years, several aspects of both so-called single- and two-stage-to-orbit space planes have provided many interesting research : Erwin Mooij. Aerospace plane can fly in the Earth's atmosphere with hypersonic and run in the low earth ing to the tactical and technical index, by adjusting power, control, pneumatic components relating to trajectory optimization, we get the optimal ascent trajectory of minimal fuel consumption at a specific separation state (height 30 km, Mach 6) with the Radaupseudospectral by: 2.
AND TRAJECTORY OPTIMIZATION NATIONAL AERONAUTICS AND SPACE ADMINISTRATION. WASHINGTON, D. C.. APRIL TECH LIBRARY KAFB, NM ‘L70 NASA CR- GUIDANCE, FLIGHT MECHANICS AND TRAJECTORY OPTIMIZATION Volume VIII - Boost Guidance Equations By G. E. Townsend, A. S. Abbott, and R. R. Palmer Flight Mechanics, and Trajectory File Size: 6MB. Mars atmospheric entry trajectory optimization via particle swarm optimization and Gauss pseudo-spectral method 23 December | Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. , No. In summary, the rescue orbit optimization problem can be described as Problem 1, where T f a u l t represents the thrust magnitude after failure. The discrete rescue flight trajectory and the optimal orbit elements corresponding to the terminal states can be jointly optimized by solving Problem 1 with a numerical optimization algorithm. Problem 1. This paper presents a trajectory optimization study that has been conducted using a recently developed tool for the synthesis and analysis of extended flight formations of long-haul commercial aircraft, with the aim to minimize overall fuel consumption. In extended flight formations, trailing aircraft can attain an appreciable reduction in induced drag and associated reduction in fuel burn by Author: Sander Hartjes, Hendrikus G. Visser, Marco E. G. van Hellenberg Hubar.