Aircraft flat-spin recovery using sliding-mode based attitude and altitude control
Author:
Affiliation:
1. Department of Aerospace Engineering, Indian Institute of Technology Kanpur, Kanpur, India
2. Defense Research and Development Organisation, Hyderabad, India
Abstract
Publisher
SAGE Publications
Subject
Mechanical Engineering,Aerospace Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/0954410020964674
Reference23 articles.
1. Inertia Coupling and Spin
2. Airplane Spin Testing
3. Abzug MJ, Larrabee EE. Airplane stability and control – a history of the technologies that made aviation possible. Cambridge, England, U.K: Cambridge Univ. Press, 1997, pp.121–142.
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