Modeling and Simulink of AutoGlide A Smart Instrument Based Aircraft Landing System
Implementation Plan:
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Step 1: Initially, we constructed a model of the aircraft with embedded sensors, including DHT11/DHT22 for humidity, HC-SR04 for altitude, RF transmitters/receivers for runway alignment, and servo-controlled landing gear.(sensors are set as like coding configurations)
Step 2: Then, we simulated the model and collected environmental and sensor data, including humidity levels, altitude readings, and RF signal strengths from the runway transmitters.
Step 3: Next, we preprocessed the collected data by filtering noise, normalizing sensor values, and calculating signal strength differences for aircraft orientation adjustments.
Step 4: Next, we applied servo control algorithms to analyze aircraft alignments and descent based on RF signal comparisons and altitude measurements based on collected data.
Step 5: Next, we analyze landing gear deployment and controlled descent when threshold altitude and alignment conditions were met based on collected sensor data.
Step 6: Finally, we evaluated performance metrics including:
6.1: Time vs Altitude (m)
6.2: Time vs Humidity (%)
6.3: Time vs RF Signal Strength (dBm)
6.4: Time vs Runway Alignment Error (m)
Software Requirements:
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1. Development Tool: MATLAB R2023a or above
2. Operating System: Windows-10 (64-bit) or above
Note:
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1) If the proposed plan does not fully align with your requirements, please provide all necessary details—including steps, parameters, models, and expected outcomes—in advance. Kindly ensure that any missing configurations or specifications are clearly outlined in the plan before confirming.
2) If there’s no built-in solution for what the project needs, we can always turn to reference models, customize our own, different math models or write the code ourselves to fulfil the process.
3) If the plan satisfies your requirement, Please confirm with us.
4) Project based on Simulation only.
