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Tuesday, May 12, 2020 | History

3 edition of Trajectory optimization for the national aerospace plane found in the catalog.

Trajectory optimization for the national aerospace plane

Trajectory optimization for the national aerospace plane

final report (June 13, 1992-October 30, 1993)

  • 313 Want to read
  • 28 Currently reading

Published by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, D.C, Springfield, Va .
Written in English

    Subjects:
  • Trajectory optimization

  • Edition Notes

    Statementprincipal investigator: Ping Lu.
    SeriesNASA contractor report -- NASA CR-194618., NASA contractor report -- NASA CR-194618.
    ContributionsUnited States. National Aeronautics and Space Administration.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL14699527M

    of the trajectory optimization required depend on the performance index, the approach and the application. This study adapts a practical optimization approach by assuming a typical structure for an aircraft trajectory and focuses on optimizing direct operating cost during cruise when the time and fuel savings are the by: A FLIGHT TRAJECTORY MODEL FOR A PC-BASED AIRSPACE ANALYSIS TOOL Ralf H. Mayer∗ The MITRE Corporation Center for Advanced Aviation System Development (CAASD) McLean, Virginia ∗ Sr. Simulation and Modeling Engineer, Member AIAA ABSTRACT This paper documents a method for rapid generation of aircraft flight by: 3.

    Manju Nag (, AE) - Trajectory Uncertainty Analysis for the Development of a Queuing Model for the National Airspace System. Kartik Kiran Parikh (, ME, jointly advised by Prof. Atilla Dogan) - CAE Tools for Modeling Inertia and Aerodynamic Properties of an R/C Airplane.   In this paper, the authors present a procedure for the global solution by the use of evolutionary algorithms of trajectory optimization and parameter estimation problems for rotorcraft vehicles. The proposed approach makes use of a novel repair heuristic based on a sequential quadratic programming method to handle problem constraints.

      The paper presents a gauss pseudospectral solution for the trajectory optimization problem of a hypersonic vehicle. Determination of optimal trajectory of a hypersonic vehicle is of great interest due to the different path and boundary conditions that need to be met for high accuracy. Recent researches show that pseudospectral methods are capable of providing high accuracy in Cited by: 4. NAP - National aerospace plane. Looking for abbreviations of NAP? It is National aerospace plane. No Additional Printings (book publishing) NAP: No Apparent Pathology (medical records) NAP: Navigation Analysis Program (US NASA) NAP: National aerospace plane; National Aerospace Standard;.


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Trajectory optimization for the national aerospace plane Download PDF EPUB FB2

The chapters of Spacecraft Trajectory Optimization are an exhibit of the current state of the art for a variety of approaches to trajectory optimization. While this is not an end-all, be-all book on the topic, it does an excellent job at explaining the different by: Trajectory optimization and guidance law development for national aerospace plane applications final report, July 1, to Novem (SuDoc NAS ) [Calise, Anthony J.] on *FREE* shipping on qualifying offers.

Trajectory optimization and guidance law development for national aerospace plane applications final report, July 1Author: Anthony J. Calise. 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.

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. APRIL TECH LIBRARY KAFB, NM ‘L70 NASA CR- GUIDANCE, FLIGHT MECHANICS AND TRAJECTORY OPTIMIZATION Volume VIII - Boost Guidance Equations By G. Townsend, A. Abbott, and 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. van Hellenberg Hubar. Betts, J. and Huffman, W. () Path-Constrained Trajectory Optimization Using Sparse Sequential Quadratic Programming Journal of Guidance, Control and Dynamics, 16, 1.

CrossRef Google Scholar Ehtamo, H.K.,T. and Hämäläinen, R.P. () A method to generate trajectories for minimum time climb, in Preprints of the 6th international Cited by: lem dependent solution procedure.

Aerospace applications and related trajectory optimization problems are an important field on which optimal control is used. This work has been carried out at the Systems Analysis Laboratory of Helsinki University of Technology in.

A Survey of Numerical Methods for Trajectory Optimization John T. Betts Mathematics and Engineering Analysis, Boeing Information and Support Services, P.O. BoxMS 7L, Seattle, Washington Aug 1Cited by:   The book begins with a simple treatment of functional optimization followed by a discussion of switching theory.

It then presents the derivation of the general equations of motion along with the basic knowledge in aerodynamics and propulsion necessary for Book Edition: 1. An inverse dynamics approach to trajectory optimization and guidance for an aerospace plane: Authors: Lu, Ping: Affiliation: AA(Iowa State University of Science and Technology, Ames) Publication: IN: AIAA Guidance, Navigation and Control Conference, Hilton Head Island, SC, Aug., Technical Papers.

1 (A ). FLIGHT TRAJECTORY OPTIMIZATION FOR AN EFFICIENT AIR TRANSPORTATION SYSTEM is an assumed sphere with radius R and the aircraft’s position is located by latitude I, longitude T 1and altitude H ¨in a polar coordinate frame XYZ. The Great Circle Route (GCR) defined as.

The ASP (Aero-Space Plane) ascent trajectory optimization is a difficult problem due to the complexity of operating the combined cycle propulsion and the absence of the enough and exact aerodynamic characteristic data during the process of calculating the dynamics model in order to achieving cargo delivery to LEO orbits.American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA Book.

Fundamentals of Aerospace Engineering; Description; Contents; Licence; Resources; Support (Donate/buy) Research. Research Team; Research topics.

Meteorological uncertainty and Air Traffic Management (ATM) Commercial aircraft trajectory optimization; Low-Thrust Trajectory Optimization; PhD Thesis Supervision. Ph. D. Thesis Daniel González.