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Comparison of Two Maneuvers for Longitudinal Range Control During Atmospheric Entry

Comparison of Two Maneuvers for Longitudinal Range Control During Atmospheric Entry PDF Author: Lionel L. Levy
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 24

Book Description


Comparison of Two Maneuvers for Longitudinal Range Control During Atmospheric Entry

Comparison of Two Maneuvers for Longitudinal Range Control During Atmospheric Entry PDF Author: Lionel L. Levy
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 24

Book Description


Comparison of Two Maneuvers for Longitudinal Range Control During Atmospheric Entry

Comparison of Two Maneuvers for Longitudinal Range Control During Atmospheric Entry PDF Author: Lionel L. Levy
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

Book Description


Comparison of Two Maneuvers for Longitudinal Range Control During Atmosphere Entry

Comparison of Two Maneuvers for Longitudinal Range Control During Atmosphere Entry PDF Author: Lionel L. Levy (Jr., & Elliott D. Katzen)
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description


Comparison of Two Maneuvers for Longitudinal Range Control During Atmosphere Entry

Comparison of Two Maneuvers for Longitudinal Range Control During Atmosphere Entry PDF Author: LIONEL L. JR. LEVY
Publisher:
ISBN:
Category :
Languages : en
Pages : 1

Book Description
ATMOSPHERE ENTRY TRAJECTORIES WERE STUDIED TO DETERMINE THE RANGE FOR TWO TYPES OF MANEUVERS. For one type range was controlled principally by varying the point in the trajectory where the lift-drag ratio was reduced to maximum negative lift-drag ratio. For the other maneuver range was controlled principally by varying the value to which the lift-drag ratio was reduced. The influence on range of maximum deceleration limit and an error in lift-drag ratio were included; the convective and radative heating to the stagnation point of the spacecraft were also studied. The analysis was made for a spacecraft with a maximum lift-drag ratio of 0.5 entering the earth's atmosphere at parabolic velocity. The results for both types of maneuvers indicate that the spacecraft aerodynamics can provide range up to global range.

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 418

Book Description


Space Rendez[v]ous, Rescue and Recovery

Space Rendez[v]ous, Rescue and Recovery PDF Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 128

Book Description


U.S. Government Research Reports

U.S. Government Research Reports PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 172

Book Description


Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1990

Book Description


Monthly Catalog of United States Government Publications, Cumulative Index

Monthly Catalog of United States Government Publications, Cumulative Index PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1284

Book Description


A Study of Synthesis Techniques for Optimal Controllers

A Study of Synthesis Techniques for Optimal Controllers PDF Author: B. Paiewonsky
Publisher:
ISBN:
Category : Automatic control
Languages : en
Pages : 204

Book Description
This report is organized as follows. A general discussion of optimal control precedes a section devoted to the mathe matical aspects of optimization. Stochastic problems are taken up next and this is followed by a section on two-point boundary problems. In many cases the main problem is to find an extreme value of a function of several variables. There is a section describing methods for doing this. The sections on synthesis procedures, computational studies and conclusions complete the main portion of the report.