Integrated Guidance and Control Using Model Predictive Control with Flight Path Angle Prediction against Pull-Up Maneuvering Target
Integrated guidance and control using model predictive control against a maneuvering target is proposed. Equations of motion for terminal homing are developed with the consideration of short-period dynamics as well as actuator dynamics of a missile. The convex optimization problem is solved consider...
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2020-06-01
|
| Series: | Sensors |
| Subjects: | |
| Online Access: | https://www.mdpi.com/1424-8220/20/11/3143 |
| _version_ | 1797566395631796224 |
|---|---|
| author | Jongho Park Youngil Kim Jong-Han Kim |
| author_facet | Jongho Park Youngil Kim Jong-Han Kim |
| author_sort | Jongho Park |
| collection | DOAJ |
| description | Integrated guidance and control using model predictive control against a maneuvering target is proposed. Equations of motion for terminal homing are developed with the consideration of short-period dynamics as well as actuator dynamics of a missile. The convex optimization problem is solved considering inequality constraints that consist of acceleration and look angle limits. A discrete-time extended Kalman filter is used to estimate the position of the target with a look angle as a measurement. This is utilized to form a flight-path angle of the target, and polynomial fitting is applied for prediction. Numerical simulation including a Monte Carlo simulation is performed to verify the performance of the proposed algorithm. |
| first_indexed | 2024-03-10T19:26:12Z |
| format | Article |
| id | doaj.art-cf6b59c7a2ba4a62950a0a6c948fd8fc |
| institution | Directory Open Access Journal |
| issn | 1424-8220 |
| language | English |
| last_indexed | 2024-03-10T19:26:12Z |
| publishDate | 2020-06-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Sensors |
| spelling | doaj.art-cf6b59c7a2ba4a62950a0a6c948fd8fc2023-11-20T02:35:05ZengMDPI AGSensors1424-82202020-06-012011314310.3390/s20113143Integrated Guidance and Control Using Model Predictive Control with Flight Path Angle Prediction against Pull-Up Maneuvering TargetJongho Park0Youngil Kim1Jong-Han Kim2Department of Military Digital Convergence, Ajou University, Suwon 16499, KoreaDepartment of Aerospace Engineering, Seoul National University, Seoul 08826, KoreaDepartment of Electronic Engineering, Kyung Hee University, Yongin 17104, KoreaIntegrated guidance and control using model predictive control against a maneuvering target is proposed. Equations of motion for terminal homing are developed with the consideration of short-period dynamics as well as actuator dynamics of a missile. The convex optimization problem is solved considering inequality constraints that consist of acceleration and look angle limits. A discrete-time extended Kalman filter is used to estimate the position of the target with a look angle as a measurement. This is utilized to form a flight-path angle of the target, and polynomial fitting is applied for prediction. Numerical simulation including a Monte Carlo simulation is performed to verify the performance of the proposed algorithm.https://www.mdpi.com/1424-8220/20/11/3143integrated guidance and controlterminal homingmodel predictive controlconvex optimization |
| spellingShingle | Jongho Park Youngil Kim Jong-Han Kim Integrated Guidance and Control Using Model Predictive Control with Flight Path Angle Prediction against Pull-Up Maneuvering Target Sensors integrated guidance and control terminal homing model predictive control convex optimization |
| title | Integrated Guidance and Control Using Model Predictive Control with Flight Path Angle Prediction against Pull-Up Maneuvering Target |
| title_full | Integrated Guidance and Control Using Model Predictive Control with Flight Path Angle Prediction against Pull-Up Maneuvering Target |
| title_fullStr | Integrated Guidance and Control Using Model Predictive Control with Flight Path Angle Prediction against Pull-Up Maneuvering Target |
| title_full_unstemmed | Integrated Guidance and Control Using Model Predictive Control with Flight Path Angle Prediction against Pull-Up Maneuvering Target |
| title_short | Integrated Guidance and Control Using Model Predictive Control with Flight Path Angle Prediction against Pull-Up Maneuvering Target |
| title_sort | integrated guidance and control using model predictive control with flight path angle prediction against pull up maneuvering target |
| topic | integrated guidance and control terminal homing model predictive control convex optimization |
| url | https://www.mdpi.com/1424-8220/20/11/3143 |
| work_keys_str_mv | AT jonghopark integratedguidanceandcontrolusingmodelpredictivecontrolwithflightpathanglepredictionagainstpullupmaneuveringtarget AT youngilkim integratedguidanceandcontrolusingmodelpredictivecontrolwithflightpathanglepredictionagainstpullupmaneuveringtarget AT jonghankim integratedguidanceandcontrolusingmodelpredictivecontrolwithflightpathanglepredictionagainstpullupmaneuveringtarget |