AIAA Guidance, Navigation, and Control Conference 2009
DOI: 10.2514/6.2009-5633
|View full text |Cite
|
Sign up to set email alerts
|

LPV Modeling, Analysis and Design in Space Systems: Rationale, Objectives and Limitations

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1
1

Citation Types

0
18
0

Year Published

2011
2011
2023
2023

Publication Types

Select...
6
1
1

Relationship

0
8

Authors

Journals

citations
Cited by 22 publications
(18 citation statements)
references
References 18 publications
0
18
0
Order By: Relevance
“…Use the choices for (Q, S, R) in (16) to rewrite the second term as e T e − γ 2 d T d. Integrate over [0, T ] to obtain:…”
Section: Robust Induced L 2 Gainmentioning
confidence: 99%
See 1 more Smart Citation
“…Use the choices for (Q, S, R) in (16) to rewrite the second term as e T e − γ 2 d T d. Integrate over [0, T ] to obtain:…”
Section: Robust Induced L 2 Gainmentioning
confidence: 99%
“…This paper develops theoretical and computational methods to analyze the robustness of linear time-varying (LTV) systems over finite time horizons. Motivating applications for this work include robotic systems [19,28] and space launch / re-entry vehicles [16,32] both of which undergo finite-time trajectories. Typical notions of robustness, e.g.…”
Section: Introductionmentioning
confidence: 99%
“…In the first phase, these techniques where tested on simpler simulation models, see [169], [171]- [174], which are therefore not included in our categorization. A more detailed overview about the project and the challenges of LPV tools in space applications can be found in [175].…”
Section: Lpv Control Applications Validated By Experiments or Himentioning
confidence: 99%
“…As a potential axis for improvement, and as briefly mentioned before, the robust control community has particularly well suited methods and tools to systematically address the aforementioned type of trade-offs, explicitly considering the effect of uncertainties and disturbances. As previously shown, these uncertainties can be modelled as time-invariant LFTs, but this formalism also allows to indirectly capture time-varying effects via linear parameter-varying (LPV) models (details on LPV modelling can be found in (Marcos & Bennani, 2009) and references therein). Furthermore, and also favoured by the use of the robust control framework, recent automated tuning tools (Apkarian & Noll, 2006;Gahinet & Apkarian, 2011) have appeared that will be able to exploit the parameterisation of the guidance laws proposed in (58) and (59) -or facilitate the synthesis of control compensators that minimise orbital perturbations with respect to a reference trajectory (Simplício et al, 2018a).…”
Section: Robustnessmentioning
confidence: 99%