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Tuesday, May 19, 2020 | History

1 edition of Performance analysis of non-coplanar synergetic maneuvers found in the catalog.

Performance analysis of non-coplanar synergetic maneuvers

Thomas P. Spriesterbach

Performance analysis of non-coplanar synergetic maneuvers

by Thomas P. Spriesterbach

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  • 38 Currently reading

Published by Naval Postgraduate School, Available from the National Technical Information Service in Monterey, Calif, Springfield, Va .
Written in English


Edition Notes

ContributionsRoss, I. Michael
The Physical Object
Pagination81 p. ;
Number of Pages81
ID Numbers
Open LibraryOL25480915M

  The present paper investigates the chaotic attitude dynamics and reorientation maneuver for completely viscous liquid-filled spacecraft with flexible appendage. All of the equations of motion are derived by using Lagrangian mechanics and then transformed into a form consisting of an unperturbed part plus perturbed terms so that the system’s nonlinear characteristics can be exploited in phase. Startup Analysis Simulator for a Small Staged Combustion–Cycle Engine Powerpack Experimental Investigation of Aerodynamic Performance of a Turbine Cascade with Trailing-Edge Injection. Jie Gao Optimization for the Aeroassisted Orbital Plane Change with the Synergetic Maneuver Using the hp-Adaptive Pseudospectral Method. Hongwei Han.

  And Haig et al., (), utilizing a DNA analysis with red-cockaded woodpeckers (Picoides borealis), found that helping behaviors involved a variety of related and unrelated birds and that there was no direct benefit to the helpers from “extra matings.” (Brown, , in a book-length synthesis on communal breeding and helping behaviors. Gao Y, Chen K () Performance analysis of precise point positioning using real-time orbit and clock products. J. GPS 3(): Gatti M An empirical method of estimation of the variance covariance matrix in GPS network design. Survey Rev. 37():

An analysis of the effect of design and measurement errors on pump performance parameters / (Washington, D.C.: National Aeronautics and Space Administration: [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia ], ), by Douglas A. Anderson, Lewis Research Center, and United States National. Abstract. Proceedings of the Second International Conference on Transportation Engineering, held in Chengdu, China, July , Sponsored by China Communications and Transportation Association; the Transportation and Development Institute of ASCE; Mao Yisheng Science and Technology Education Fund.


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Performance analysis of non-coplanar synergetic maneuvers by Thomas P. Spriesterbach Download PDF EPUB FB2

The term synergetic was coined to describe the combination of propulsive and atmospheric forces used by a maneuvering flight vehicle. This thesis concentrates on non-coplanar synergetic maneuvers using two different control methods for various lifting bodies.

The term synergetic has been coined to describe to combination of propulsive and atmospheric forces used by a maneuvering flight vehicle. This thesis concentrates on non-coplanar synergetic maneuvers using two different control methods for various lifting bodies over a range of heating rates and orbital : Thomas P.

Spriesterbach. methods. The term synergetic has been coined to describe the combination of propulsive and atmospheric forces used by a maneuvering flight vehicle. This thesis concentrates on non-coplanar synergetic maneuvers using two different control methods for various lifting bodies over a range of heating rates and orbital speeds.

Anevaluation,analysis,andcomparisonofthetwomaneuversovera range of maximum lift to drag ratios ((L/D) max) and heating rateswill shed light on thecapabilities andinadequaciesofeach control method. in a non-coplanar o rbit different fro m the two deputy satellites. The configuration of formation for these satellites is the projected circular orbit (PCO) type with the phase angle difference.

Performance analysis of non-coplanar synergetic maneuvers book for the Aeroassisted Orbital Plane Change with the Synergetic Maneuver Using the hp-Adaptive Pseudospectral Method Journal of Aerospace Engineering, Vol.

30, No. 6 Identifying method of entry and exit conditions for aerocapture with near minimum fuel consumption. Synergetic control technique is adopted to derive tracking controller first which is dependent on inertia matrix.

The controller is then redesigned to be adaptive by estimation of inertia parameters. of transferring from one orbit to another by impulsive delta-v maneuvers, including Hohmanntransfers,phasingorbitsandplanechanges. Chapter7derivesandemploys the equations of relative motion required to understand and design two-impulse ren-dezvous maneuvers.

Chapter 8 explores the basics of interplanetary mission analysis. M.K. Paul, and S.I. Roumeliotis, "Alternating-Stereo VINS: Observability Analysis and Performance Evaluation," IEEE Conference on Computer Vision and Pattern Recognition (CVPR'18), Salt Lake City, UT, June C   eBook is an electronic version of a traditional print book that can be read by using a personal computer or by using an eBook reader.

force system Concurrent/ non concurrent Co-linear / non co-linear parallel./ non parallel Like / unlike parallel Non coplanar force system Nilesh G. such as analysis of forces on a beam. 04 Twisting. E. Dickmann, The effect of finite thrust and heating constraints on the synergetic plane change maneuver for space-shuttle orbiter-class vehicle, NASA TN D.

American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA 1. Introduction. Orbital rendezvous and interception belong to significant orbital maneuvers, such as the spatial on-orbit service, spatial emergency rescue mission, and debris removal [,, ].These orbital maneuvers consume high amount of fuel [7,8].This characteristic will directly weaken the spacecraft performance in subsequent spatial missions, such as orbital maintenance and.

A relative dynamics equation-set based on orbital element differences with J 2 effects is derived, based on which a two-level approach is proposed to optimize the Mars orbital rendezvous phasing with a large difference in the initial ascending node.

The up-level problem uses the revolution deviation between the target spacecraft and the chaser as the design variable, and employs a linear. The proposed work introduces an enhanced concept in Bloom filter called Bin Bloom Filter (BBF). The performance of BBF over conventional Bloom filter is evaluated under various optimization techniques.

Real time data set and synthetic data sets are used for experimental analysis and the results are demonstrated for bin sizes 4, 5, 6 and 7. The same method used to solve coplanar concurrent force systems is used to solve non-coplanar concurrent systems. The plane-table (an early surveying instrument) weighs 40 pounds and is supported by a tripod, the legs of which are pushed into the ground.

The force in each leg may be considered to act along the leg. III European Conference on Computational Mechanics: Solids, Structures and Coupled Problem in Engineering Computational Mechanics in Solid, Structures and Coupled Problems in Engineering is today a mature science with applications to major industrial projects.

This book contains the edited version. Executing a non-coplanar transfer requires more fuel than an orbital change within the original plane, such as increasing or decreasing orbital velocity to change orbital radius or altitude.

In addition to velocity changes, a non-coplanar transfer requires a change in the direction of travel 0 of the spacecraft. Advanced Microsystems for Automotive Applications Smart Systems for Safe and Green Vehicles | Andreas von Eichhorn, Peter Zahn, Dieter Schramm (auth.), Jan Fischer-Wolfarth, Gereon Meyer (eds.) | download | B–OK.

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The. Examples from engineering mechanics. Discover Resources. Rolle's Theorem; Writing Equations to Represent Tables Sequential quadratic programming (SQP) methods have proved highly effective for solving constrained optimization problems with smooth nonlinear functions in the objective and constraints.

() Optimization for the Aeroassisted Orbital Plane Change with the Synergetic Maneuver Using the hp-Adaptive Pseudospectral Method. () Time.5. Non Coplanar concurrent force system. F1. F2. F3. 6. Non Coplanar non concurrent force system Dr. G.

Amaranath, BITS Pilani, Dubai Campus Dr. G. Amaranath, BITS Pilani, Dubai Campus Dr. G. Amaranath, BITS Pilani, Dubai Campus MOMENT The tendency of a force is not only to move the body but also to rotate the body.