2007
DOI: 10.2514/1.27758
|View full text |Cite
|
Sign up to set email alerts
|

Adaptive, Integrated Guidance and Control Design for Line-of-Sight-Based Formation Flight

Abstract: This paper presents an integrated guidance and control design for formation flight using a combination of adaptive output feedback and backstepping techniques without an underlying timescale separation assumption. We formulate the problem as an adaptive output feedback control problem for a line-of-sight (LOS) based formation flight configuration of a leader and a follower aircraft. The design objective is to regulate range and two bearing angle rates while maintaining turn coordination. Adaptive neural networ… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1

Citation Types

0
12
0

Year Published

2007
2007
2022
2022

Publication Types

Select...
8
1

Relationship

1
8

Authors

Journals

citations
Cited by 28 publications
(12 citation statements)
references
References 16 publications
0
12
0
Order By: Relevance
“…where the bounds on with the normal form given by (3), let the adaptive estimator be given by (12), the adaptive control law by (30), (31), the observer NN adaptive law by (25), and the controller NN adaptive law by (44). Then the closed-loop system errors ζ are uniformly ultimately bounded.…”
Section: Lyapunov-like Stability Analysismentioning
confidence: 99%
See 1 more Smart Citation
“…where the bounds on with the normal form given by (3), let the adaptive estimator be given by (12), the adaptive control law by (30), (31), the observer NN adaptive law by (25), and the controller NN adaptive law by (44). Then the closed-loop system errors ζ are uniformly ultimately bounded.…”
Section: Lyapunov-like Stability Analysismentioning
confidence: 99%
“…The adaptive control solution is based on the adaptive IGC design presented in Ref. [12]. Finally, simulation results using a nonlinear 6DOF simulation model of a fixed-wing UAV are presented.…”
mentioning
confidence: 99%
“…Kim et al presented an integrated guidance and control design for formation flight using a combination of adaptive controllers. 11 This paper assumed uncertainties resulting from unknown leader aircraft's acceleration and modeling error due to parametric uncertainties.…”
Section: Introductionmentioning
confidence: 99%
“…However, in Sattigeri et al, 15 a three-dimensional formation flight simulation is proposed in which an adaptive acceleration-based guidance law is designed for the purpose of tracking a maneuvering leader aircraft. Moreover, in Kim et al, 16 a combination of adaptive output feedback and backstepping techniques is used for a line of sight-based formation flight configuration of a leader and a follower aircraft. In Ryoo et al, 17 optimal guidance laws for multiple vehicles formation flight are addressed and a method to compensate the acceleration or maneuver of the formation leader is included in the guidance laws.…”
Section: Introductionmentioning
confidence: 99%