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Estimation of the local attitude of orbiting spacecraft

  • Published:1971-03 Issue:2 Volume:7 Page:163-180
  • ISSN:0005-1098
  • Container-title:Automatica
  • language:en
  • Short-container-title:Automatica

Author:

Bryson A.E.,Kortüm W.

Publisher

Elsevier BV

Subject

Electrical and Electronic Engineering,Control and Systems Engineering

Reference38 articles.

1. Spacecraft attitude determination symposium,1969

2. Inertial Guidance;Pitman,1962

3. Performance of strapdown inertial attitude reference systems;Farrell;AIAA Journal Spacecraft Rockets,1966

4. Two approaches to the starmapping problem for space vehicle attitude determination;Gorstein,1969

5. Sub-arc second star sensors, design and fabrication;Carroll,1969

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1. Development of the algorithm of the spacecraft programmed yaw turns with the use of orbital gyrocompass;XLIII ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration;2019

2. Micro-Satellite Attitude Determination with Only a Single Horizon Sensor;MATEC Web of Conferences;2016

3. Flexible spacecraft attitude measurement and control scheme incorporating state estimation;Optimal Control Applications and Methods;2007-10-29

4. Observability of a Geosynchronous Spacecraft Attitude Determination System;Journal of Guidance, Control, and Dynamics;2003-11

5. Notes on Observability of Geosynchronous Spacecraft Attitude Determination System;AIAA Guidance, Navigation, and Control Conference and Exhibit;2002-06-25
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