PARAMETRIC OPTIMIZATION OF AUGMENTED PROPORTIONAL NAVIGATION LAW CONSIDERING PERFORMANCE AND MANEUVERING CAPABILITIES

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AZIZI AMIR; Karimi Jalal; SADATI SEYED HOSSEIN

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Journal: JOURNAL OF AERONAUTICAL ENGINEERING (JOAE) Year:2015 | Volume:17 | Issue:1 Page(s): 67-76

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Title

PARAMETRIC OPTIMIZATION OF AUGMENTED PROPORTIONAL NAVIGATION LAW CONSIDERING PERFORMANCE AND MANEUVERING CAPABILITIES

Author(s)

AZIZI AMIR | Karimi Jalal | SADATI SEYED HOSSEIN | Issue Writer Certificate

Keywords

INTEGRATED GUIDANCE AND CONTROLQ2

AUGMENTED PROPORTIONAL NAVIGATIONQ2

PERFORMANCE CONSTRAINTSQ2

MULTIQ2

OBJECTIVE OPTIMIZATIONQ2

Abstract

The aerial vehicle performance capabilities are usually ignored during the guidance laws design. This may result in saturation of commands and undesirable behavior of INTEGRATED GUIDANCE AND CONTROL system. In the current research, based on the AUGMENTED PROPORTIONAL NAVIGATION (APN) law and considering the performance and maneuvering capabilities of a flying vehicle through different flight conditions, the parameters of APN are optimized. In contrast with the conventional APN, in the proposed guidance law, the guidance parameters are not fixed but are functions of environmental conditions and engagement scenarios. In this regard, utilizing different flight conditions and engagement scenarios, a MULTI-objective optimization problem is formed. The performance and maneuvering capabilities are considered as the optimization constraints. MULTI-objective problem includes three objectives of miss distance, acceleration command and flight time. The NSGA-II algorithm is utilized here. The limits of the acceleration commands are not fixed and vary depending on the flight conditions. The simulation of several scenarios, reveals a superior behavior for the proposed guidance law in comparison with the conventional laws.

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APA: Copy

AZIZI, AMIR, Karimi, Jalal, & SADATI, SEYED HOSSEIN. (2015). PARAMETRIC OPTIMIZATION OF AUGMENTED PROPORTIONAL NAVIGATION LAW CONSIDERING PERFORMANCE AND MANEUVERING CAPABILITIES. JOURNAL OF AERONAUTICAL ENGINEERING (JOAE), 17(1), 67-76. SID. https://sid.ir/paper/173100/en

Vancouver: Copy

AZIZI AMIR, Karimi Jalal, SADATI SEYED HOSSEIN. PARAMETRIC OPTIMIZATION OF AUGMENTED PROPORTIONAL NAVIGATION LAW CONSIDERING PERFORMANCE AND MANEUVERING CAPABILITIES. JOURNAL OF AERONAUTICAL ENGINEERING (JOAE)[Internet]. 2015;17(1):67-76. Available from: https://sid.ir/paper/173100/en

IEEE: Copy

AMIR AZIZI, Jalal Karimi, and SEYED HOSSEIN SADATI, “PARAMETRIC OPTIMIZATION OF AUGMENTED PROPORTIONAL NAVIGATION LAW CONSIDERING PERFORMANCE AND MANEUVERING CAPABILITIES,” JOURNAL OF AERONAUTICAL ENGINEERING (JOAE), vol. 17, no. 1, pp. 67–76, 2015, [Online]. Available: https://sid.ir/paper/173100/en

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