Re-entry Flight Controller Design using Nonlinear Dynamic Inversion. AIAA 2001-4219

R da Costa, QP Chu, JA Mulder

Research output: Chapter in Book/Conference proceedings/Edited volumeConference contributionScientificpeer-review

Original languageUndefined/Unknown
Title of host publicationAIAA proceedings on Guidance, Navigation and Control
Place of PublicationNew York
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
Pages21-32
Number of pages12
Publication statusPublished - 2001
EventAIAA Guidance Navigation and Control Conference, Montreal, Canada - New York
Duration: 6 Aug 2001 → …

Publication series

Name
PublisherAIAA

Conference

ConferenceAIAA Guidance Navigation and Control Conference, Montreal, Canada
Period6/08/01 → …

Keywords

  • ZX Int.klas.verslagjaar < 2002

Cite this

da Costa, R., Chu, QP., & Mulder, JA. (2001). Re-entry Flight Controller Design using Nonlinear Dynamic Inversion. AIAA 2001-4219. In AIAA proceedings on Guidance, Navigation and Control (pp. 21-32). American Institute of Aeronautics and Astronautics Inc. (AIAA).