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 proceeding › Conference Contribution (Conference Proceeding)

2 Citations (Scopus)

Original language	English
Title of host publication	AIAA Guidance, Navigation & Control Conference, USA
Pages	584 - 594
Number of pages	11
Publication status	Published - Aug 2004

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)

@inproceedings{6b7fc4b9427a47ac873e07a8fab3549f,

title = "Continuation methods for aircraft models subject to integrator wind-up",

author = "TS Richardson and DP Stoten and MH Lowenberg and {Di Bernardo}, M",

note = "Other identifier: AIAA_2004-4946",

year = "2004",

month = aug,

language = "English",

pages = "584 -- 594",

booktitle = "AIAA Guidance, Navigation & Control Conference, USA",

}