From Flight Test to a Simulator Model - System Identification of the ISTAR Research Aircraft

The German Aerospace Centre (DLR) acquired a Dassault Falcon 2000LX research aircraft, designated ISTAR (In-flight Systems & Technology Airborne Research), to support research in variable stability, advanced flight control concepts, and pilot assistance systems. A high-fidelity flight dynamics model of the ISTAR is essential for the development of these systems and for simulator-based flight control testing. The model is based on an aerodynamic model identified through system identification (SysID) techniques using flight test data. The modular design of the aerodynamic modelling software enabled seamless integration of the identified model into the ISTAR simulator. This paper gives an overview of the model development process and an example for the application of the simulator model for the design and implementation of a yaw controller is presented.

Authors

Publication Details

Journal
elib (German Aerospace Center)
Published
2025-12-04
Primary Topic
Aerospace and Aviation Technology
Type
article
Field-Weighted Citation Impact
0.00
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

From Flight Test to a Simulator Model - System Identification of the ISTAR Research Aircraft

Anton Dilcher, Christian Raab
elib (German Aerospace Center)
Aerospace and Aviation Technology
article

From Flight Test to a Simulator Model - System Identification of the ISTAR Research Aircraft

Anton Dilcher, Christian Raab
article en

Abstract

The German Aerospace Centre (DLR) acquired a Dassault Falcon 2000LX research aircraft, designated ISTAR (In-flight Systems & Technology Airborne Research), to support research in variable stability, advanced flight control concepts, and pilot assistance systems. A high-fidelity flight dynamics model of the ISTAR is essential for the development of these systems and for simulator-based flight control testing. The model is based on an aerodynamic model identified through system identification (SysID) techniques using flight test data. The modular design of the aerodynamic modelling software enabled seamless integration of the identified model into the ISTAR simulator. This paper gives an overview of the model development process and an example for the application of the simulator model for the design and implementation of a yaw controller is presented.

elib (German Aerospace Center)
Openalex Percentile: Top 15%
Aerospace and Aviation Technology
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.