Simulation of Launch Pad Atomization for Military Weapon System

This study aims to optimize three critical parameters (inclination angle, hook lifting, and sparking) for a missile launching system by combining precise mathematical methods, IoT concepts, and advanced sensor technologies. The system uses an Inertial Navigation System (INS) in conjunction with gyro and proximity sensors to ensure accurate target interception by carefully determining the optimal launch angle. The Internet of Things concept is integrated effortlessly, with a clever coordinating WiFi networking, weight estimation, and sensor data processing for real-time cloud data flow. Security protocols protect the integrity of the data, and a reliable power supply system guarantees reliable operation. The project incorporates both Hot Start and Cold Start functionalities, enabling dependable launches and prompt adaptations to dynamic changes. Flexible igniting mechanisms such as Chemical, Electrical, and Electro-Chemical systems are available, and reliable and secure missile launches are prioritized with safety features like Spark Damping Inner Tube Coating and Moisture-Resistant igniting. All things considered, this project prioritizes security, dependability, and adaptability while addressing critical elements required for a sophisticated and efficient missile launching system.

Authors

Publication Details

Journal
Communications on Applied Nonlinear Analysis
Published
2024-10-19
DOI
https://doi.org/10.52783/cana.v32.2011
Primary Topic
Rocket and propulsion systems research
Type
article
Field-Weighted Citation Impact
0.00
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article

Simulation of Launch Pad Atomization for Military Weapon System

Vijaya N. Aher
Communications on Applied Nonlinear Analysis
Rocket and propulsion systems research
article

Simulation of Launch Pad Atomization for Military Weapon System

Vijaya N. Aher
article en

Abstract

This study aims to optimize three critical parameters (inclination angle, hook lifting, and sparking) for a missile launching system by combining precise mathematical methods, IoT concepts, and advanced sensor technologies. The system uses an Inertial Navigation System (INS) in conjunction with gyro and proximity sensors to ensure accurate target interception by carefully determining the optimal launch angle. The Internet of Things concept is integrated effortlessly, with a clever coordinating WiFi networking, weight estimation, and sensor data processing for real-time cloud data flow. Security protocols protect the integrity of the data, and a reliable power supply system guarantees reliable operation. The project incorporates both Hot Start and Cold Start functionalities, enabling dependable launches and prompt adaptations to dynamic changes. Flexible igniting mechanisms such as Chemical, Electrical, and Electro-Chemical systems are available, and reliable and secure missile launches are prioritized with safety features like Spark Damping Inner Tube Coating and Moisture-Resistant igniting. All things considered, this project prioritizes security, dependability, and adaptability while addressing critical elements required for a sophisticated and efficient missile launching system.

Communications on Applied Nonlinear AnalysisVol. 32(3)
Affordable and clean energy
Openalex Percentile: Top 68%
Rocket and propulsion systems research
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Simulation of Launch Pad Atomization for Military Weapon System — Vijaya N. Aher · Communications on Applied Nonlinear Analysis (2024) | TGRS Research Map | TGRS