Iterative computation of initial quaternion-Reference-Cited by-同舟云学术

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Iterative computation of initial quaternion

Published:1970-03 Issue:3 Volume:7 Page:367-369
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

BAR-ITZHACK ITZHACK Y.¹

Affiliation:

1. Bellcomm Inc., Washington, D.C.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.29944

Reference9 articles.

1. An attitude control system for large launch vehicles.

2. Siljak, D., Nonlinear Systems, Wiley, New York, 1969, pp.152-171and 177-186.

3. Wiener, T. F. "Theoretical Analysis of Gimballess Inertial Reference Equipment Using Delta Modulated Instruments," Ph.D. dissertation,1962, Massachusetts Institute of Technology.

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Ballistic missile trajectory prediction using a state transition matrix;Applied Mathematics and Computation;2007-05

2. Review of Attitude Representations Used for Aircraft Kinematics;Journal of Aircraft;2001-07

3. A review of attitude kinematics for aircraft flight simulation;Modeling and Simulation Technologies Conference;2000-08-14

4. Strapdown Navigation Technology: A Literature Survey;Journal of Guidance and Control;1978-05

5. Strapdown navigation technology - A literature survey;Guidance and Control Conference;1977-08-08

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