2012 IEEE 51st IEEE Conference on Decision and Control (CDC) 2012
DOI: 10.1109/cdc.2012.6426709
|View full text |Cite
|
Sign up to set email alerts
|

Multiphase mixed-integer optimal control framework for aircraft conflict avoidance

Abstract: This paper formulates the problem of aircraft conflict avoidance as a multiphase mixed-integer optimal control problem. In order to find optimal maneuvers, accurate models of aircraft nonlinear dynamics and flight envelop constraints are used. Wind forecast and obstacles in airspace due to hazardous weather are included. The objective is to design aircraft maneuvers that ensure safety while minimizing fuel consumption. The solution approach is based on conversion of the multiphase mixed-integer optimal control… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
2
1

Citation Types

0
6
0

Year Published

2014
2014
2020
2020

Publication Types

Select...
2
2
1

Relationship

2
3

Authors

Journals

citations
Cited by 5 publications
(6 citation statements)
references
References 25 publications
0
6
0
Order By: Relevance
“…Different gait patterns can be represented by toggling the binary values of Λ i . The time t is discretized using a variable time-step parameterization [32], where each phase has the same number of integration nodes (blue and purple dots) that scale proportionally with respect to the switching timet i .…”
Section: B Minlp Optimal Control Formulationmentioning
confidence: 99%
“…Different gait patterns can be represented by toggling the binary values of Λ i . The time t is discretized using a variable time-step parameterization [32], where each phase has the same number of integration nodes (blue and purple dots) that scale proportionally with respect to the switching timet i .…”
Section: B Minlp Optimal Control Formulationmentioning
confidence: 99%
“…(MIOCP) By discretizing the problem at this stage, one obtains a MINLP [27]. This results in n q binary decision variables for each discretization step and thus, the problem becomes intractable for more than a few number of discrete modes.…”
Section: A Formulation As Miocpmentioning
confidence: 99%
“…We use is the so-called Hermite-Simpson direct collocation method [40]. It has been widely used for solving optimal control problems in aircraft and aerospace applications due to its computational efficiency [43], [27].…”
Section: Formulation As a Nonlinear Programmentioning
confidence: 99%
See 1 more Smart Citation
“…Given the switching sequence and times, the third subtask is a regular optimal control problem with a finite number of discontinuities in the system vector field. The necessary condition of optimality in the context of hybrid systems has been derived from Pontryagin's maximum principle (Branicky et al, 1998;Sussmann, 1999;Riedinger et al, 2003) and subsequently, various computational techniques have been developed to solve this problem (Shaikh and Caines, 2007;Soler et al, 2012;Pakniyat and Caines, 2014).…”
Section: Introductionmentioning
confidence: 99%