A Method for Longitudinal and Lateral Range Control for a High-drag Low-lift Vehicle Entering the Atmosphere of a Rotating Earth

A Method for Longitudinal and Lateral Range Control for a High-drag Low-lift Vehicle Entering the Atmosphere of a Rotating Earth PDF Author: John Worth Young
Publisher:
ISBN:
Category : Trajectories
Languages : en
Pages : 32

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Book Description
A study has been made of a method for controlling the trajectory of a high-drag low-lift entry vehicle to a desired longitude and latitude on the surface of a rotating earth. By use of this control technique the vehicle can be guided to the desired point when the present position and heading of the vehicle are known and the desired longitude and latitude are specified. The present study makes use of a single reference trajectory and an estimate of the lift and side-force capabilities of the vehicle. This information is stored in a control-logic system and used with linear control equations to guide the vehicle to the desired destination. Results are presented of a number of trajectory studies which describe the operation of the control system and illustrate its ability to control the vehicle trajectory to the desired landing area.

A Method for Longitudinal and Lateral Range Control for a High-drag Low-lift Vehicle Entering the Atmosphere of a Rotating Earth

A Method for Longitudinal and Lateral Range Control for a High-drag Low-lift Vehicle Entering the Atmosphere of a Rotating Earth PDF Author: John Worth Young
Publisher:
ISBN:
Category : Trajectories
Languages : en
Pages : 32

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Book Description
A study has been made of a method for controlling the trajectory of a high-drag low-lift entry vehicle to a desired longitude and latitude on the surface of a rotating earth. By use of this control technique the vehicle can be guided to the desired point when the present position and heading of the vehicle are known and the desired longitude and latitude are specified. The present study makes use of a single reference trajectory and an estimate of the lift and side-force capabilities of the vehicle. This information is stored in a control-logic system and used with linear control equations to guide the vehicle to the desired destination. Results are presented of a number of trajectory studies which describe the operation of the control system and illustrate its ability to control the vehicle trajectory to the desired landing area.

NASA Technical Report

NASA Technical Report PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 930

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NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 394

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Proceedings of the Optimum System Synthesis Conference, 11-13 September 1962

Proceedings of the Optimum System Synthesis Conference, 11-13 September 1962 PDF Author:
Publisher:
ISBN:
Category : Automatic control
Languages : en
Pages : 412

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Book Description
The proceedings contain a collection of 16 papers presented at the Optimum System Synthesis Conference held at the Aeronautical Systems Division 11 - 13 September 1962. The meeting was directed toward defining the present position of optimum synthesis and determining guides for future research in both applications and theory. Most papers are concerned with various aspects of recent applications and theoretical developments in optimal control such as steepest descent techniques, suboptimal controllers, optimum filtering, and functional analysis techniques. Some earlier results are also discussed.

Index of N A S A Technical Publications

Index of N A S A Technical Publications PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages : 448

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 450

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Guidance and Control II

Guidance and Control II PDF Author: Robert Langford
Publisher: Elsevier
ISBN: 032314182X
Category : Technology & Engineering
Languages : en
Pages : 1014

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Book Description
Guidance and Control - II focuses on the techniques and processes involved relative to the control of rockets, missiles, and other space vehicles. Divided into seven parts with 36 chapters, the book focuses first on active and passive control for space vehicles; advances in attitude control; the stabilization of earth satellites; and the theoretical and practical considerations of solar pressure attitude control for interplanetary space vehicles. The compilation also notes the use of gyrostabilizers on satellites, including the use of two-pulse attitude control and bank angle control for an asymmetric spinning satellite. Experiments on gyro rotor imbalance on a stable platform and various navigation and guidance systems are also presented. The book also looks at the use of sensors, the stellar techniques for interplanetary flights, and control of space vehicles. The text also gives emphasis on various mathematical equations used to measure fuel optimization in orbital rendezvous. Guidance techniques in lunar landing are also discussed. The compilation is important for readers interested in studying the methods, principles, and processes involved in the control of space vehicles.

Monthly Catalog of United States Government Publications

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

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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

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CONTROL, GUIDANCE, AND NAVIGATION OF SPACECRAFT

CONTROL, GUIDANCE, AND NAVIGATION OF SPACECRAFT PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 72

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