Continuation methods for aircraft models subject to integrator wind-up

TS Richardson, DP Stoten, MH Lowenberg, M Di Bernardo

Research output: Chapter in Book/Report/Conference proceedingConference Contribution (Conference Proceeding)

2 Citations (Scopus)
Original languageEnglish
Title of host publicationAIAA Guidance, Navigation & Control Conference, USA
Pages584 - 594
Number of pages11
Publication statusPublished - Aug 2004

Bibliographical note

Other identifier: AIAA_2004-4946

Cite this

Richardson, TS., Stoten, DP., Lowenberg, MH., & Di Bernardo, M. (2004). Continuation methods for aircraft models subject to integrator wind-up. In AIAA Guidance, Navigation & Control Conference, USA (pp. 584 - 594)