Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301) 2002
DOI: 10.1109/acc.2002.1024494
|View full text |Cite
|
Sign up to set email alerts
|

Optimal aircraft control upset recovery with and without component failures

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

0
5
0

Year Published

2010
2010
2023
2023

Publication Types

Select...
5

Relationship

0
5

Authors

Journals

citations
Cited by 6 publications
(5 citation statements)
references
References 1 publication
0
5
0
Order By: Relevance
“…Genetic algorithms 12 have been used to find the optimal recovery guidance law. Sparks et al 13 modify the guidance law to minimize altitude loss, showing that a Boeing 737-300 crash could have been prevented. These methods are computationally expensive and do not inherently prevent upsets.…”
Section: Iia Backgroundmentioning
confidence: 98%
“…Genetic algorithms 12 have been used to find the optimal recovery guidance law. Sparks et al 13 modify the guidance law to minimize altitude loss, showing that a Boeing 737-300 crash could have been prevented. These methods are computationally expensive and do not inherently prevent upsets.…”
Section: Iia Backgroundmentioning
confidence: 98%
“…In this paper, we develop an MPC strategy to minimize loss-of-altitude using only the elevator η, i.e., thrust F = 0, in accordance with governmental procedures for manual recovery [30]. LOA is a crucial metric for both collision avoidance and operating envelope recovery post stabilization [11,12]. We will adopt the convention that the aircraft has recovered when it returns to a stable trim condition within the region of attraction of a nominal flight controller which subsequently reinstates level flight.…”
Section: Problem Formulationmentioning
confidence: 99%
“…the stage cost . Proving this condition requires a suitable storage function Λ : X → R satisfying (11). With an analytical search for Λ being intractable in general, a polynomial storage function proving dissipativity can invariant subset ellipsoidal shape trim condition 0 actuator rate (°/s) be synthesized by solving a sum-of-squares feasibility problem.…”
Section: A Dissipativity and Regularizationmentioning
confidence: 99%
See 2 more Smart Citations