How to Calculate How Much Weight a Drone Can Carry

Drone Payload Calculator: How Much Weight Can Your Drone Carry? :root { –primary-color: #004a99; –success-color: #28a745; –background-color: #f8f9fa; –text-color: #333; –secondary-text-color: #555; –border-color: #ddd; –shadow-color: rgba(0, 0, 0, 0.1); –input-bg: #fff; –button-bg: var(–primary-color); –button-hover-bg: #003366; –error-color: #dc3545; } body { font-family: 'Segoe UI', Tahoma, Geneva, Verdana, sans-serif; background-color: var(–background-color); color: var(–text-color); line-height: 1.6; margin: 0; padding: 0; display: flex; flex-direction: column; align-items: center; } main { width: 100%; max-width: 1000px; margin: 20px auto; padding: 20px; background-color: #fff; box-shadow: 0 4px 12px var(–shadow-color); border-radius: 8px; display: flex; flex-direction: column; gap: 30px; } h1, h2, h3 { color: var(–primary-color); text-align: center; } h1 { font-size: 2.5em; margin-bottom: 10px; } h2 { font-size: 1.8em; margin-top: 20px; margin-bottom: 15px; } h3 { font-size: 1.4em; margin-top: 15px; margin-bottom: 10px; } p { margin-bottom: 15px; } .calculator-container { border: 1px solid var(–border-color); border-radius: 8px; padding: 30px; background-color: var(–background-color); box-shadow: inset 0 2px 6px var(–shadow-color); } .input-group { margin-bottom: 20px; text-align: left; } .input-group label { display: block; margin-bottom: 8px; font-weight: bold; color: var(–primary-color); } .input-group input[type="number"], .input-group select { width: calc(100% – 22px); padding: 12px; border: 1px solid var(–border-color); border-radius: 5px; box-sizing: border-box; font-size: 1em; color: var(–text-color); background-color: var(–input-bg); } .input-group input[type="number"]:focus, .input-group select:focus { border-color: var(–primary-color); outline: none; box-shadow: 0 0 0 3px rgba(0, 74, 153, 0.2); } .input-group small { display: block; margin-top: 8px; font-size: 0.9em; color: var(–secondary-text-color); } .error-message { color: var(–error-color); font-size: 0.85em; margin-top: 5px; display: none; /* Hidden by default */ } .error-message.visible { display: block; } .button-group { display: flex; justify-content: space-between; margin-top: 25px; gap: 15px; } button { padding: 12px 25px; border: none; border-radius: 5px; cursor: pointer; font-size: 1em; font-weight: bold; transition: background-color 0.3s ease; color: white; flex: 1; } button.primary { background-color: var(–button-bg); } button.primary:hover { background-color: var(–button-hover-bg); } button.secondary { background-color: var(–secondary-text-color); } button.secondary:hover { background-color: #444; } .result-container { margin-top: 30px; padding: 25px; border: 1px solid var(–border-color); border-radius: 8px; background-color: var(–primary-color); color: white; text-align: center; box-shadow: 0 4px 8px var(–shadow-color); } .result-container h2 { color: white; margin-bottom: 15px; } .main-result { font-size: 2.5em; font-weight: bold; margin-bottom: 10px; } .result-details { font-size: 1.1em; color: rgba(255, 255, 255, 0.9); } .result-details span { font-weight: bold; } .results-explanation { font-size: 0.9em; margin-top: 15px; color: rgba(255, 255, 255, 0.8); } .intermediate-results { margin-top: 20px; padding: 20px; border-radius: 6px; background-color: rgba(255, 255, 255, 0.1); display: flex; flex-wrap: wrap; justify-content: center; gap: 20px; } .intermediate-results div { text-align: center; padding: 10px 15px; border-right: 1px solid rgba(255, 255, 255, 0.3); } .intermediate-results div:last-child { border-right: none; } .intermediate-results span { display: block; font-size: 1.8em; font-weight: bold; color: white; } .intermediate-results p { margin: 0; font-size: 0.95em; color: rgba(255, 255, 255, 0.8); } .chart-container { margin-top: 30px; padding: 25px; border: 1px solid var(–border-color); border-radius: 8px; background-color: #fff; box-shadow: 0 4px 8px var(–shadow-color); } .chart-container h3 { margin-bottom: 20px; color: var(–primary-color); } #payloadChart { width: 100%; height: 350px; } .chart-legend { text-align: center; margin-top: 15px; font-size: 0.9em; color: var(–secondary-text-color); } .chart-legend span { display: inline-block; margin: 0 10px; } .chart-legend .legend-color { display: inline-block; width: 15px; height: 15px; margin-right: 5px; border-radius: 3px; vertical-align: middle; } .table-container { margin-top: 30px; padding: 25px; border: 1px solid var(–border-color); border-radius: 8px; background-color: #fff; box-shadow: 0 4px 8px var(–shadow-color); overflow-x: auto; } .table-container h3 { margin-bottom: 20px; color: var(–primary-color); } table { width: 100%; border-collapse: collapse; margin-top: 15px; } th, td { padding: 12px 15px; text-align: left; border-bottom: 1px solid var(–border-color); } thead { background-color: var(–primary-color); color: white; } th { font-weight: bold; } tbody tr:hover { background-color: rgba(0, 74, 153, 0.08); } caption { caption-side: top; font-weight: bold; font-size: 1.2em; color: var(–primary-color); margin-bottom: 10px; text-align: left; } .article-section { margin-top: 40px; padding: 30px; border: 1px solid var(–border-color); border-radius: 8px; background-color: #fff; box-shadow: 0 4px 8px var(–shadow-color); text-align: left; } .article-section h2 { text-align: left; margin-bottom: 20px; border-bottom: 2px solid var(–primary-color); padding-bottom: 5px; } .article-section h3 { text-align: left; margin-top: 25px; margin-bottom: 10px; color: var(–primary-color); } .article-section p, .article-section ul, .article-section ol { margin-bottom: 15px; color: var(–text-color); } .article-section ul, .article-section ol { padding-left: 20px; } .article-section li { margin-bottom: 8px; } .article-section strong { color: var(–primary-color); } .internal-links-list { list-style: none; padding: 0; } .internal-links-list li { margin-bottom: 15px; } .internal-links-list a { color: var(–primary-color); font-weight: bold; text-decoration: none; } .internal-links-list a:hover { text-decoration: underline; } .internal-links-list span { display: block; font-size: 0.9em; color: var(–secondary-text-color); margin-top: 5px; } footer { text-align: center; padding: 20px; margin-top: 40px; font-size: 0.9em; color: var(–secondary-text-color); width: 100%; } @media (max-width: 768px) { h1 { font-size: 2em; } h2 { font-size: 1.5em; } h3 { font-size: 1.2em; } main { padding: 15px; } .calculator-container, .result-container, .chart-container, .table-container, .article-section { padding: 20px; } .button-group { flex-direction: column; } button { width: 100%; } .intermediate-results div { border-right: none; padding: 10px 0; width: 100%; } }

Drone Payload Calculator

Determine the maximum weight your drone can safely carry.

Calculate Drone Carrying Capacity

The weight of the drone itself without any payload or battery.
The weight of the fully charged battery.
The maximum lifting force each individual motor can produce (kilogram-force).
4 (Quadcopter) 6 (Hexacopter) 8 (Octocopter) Select the number of motors on your drone.
A multiplier to ensure safe operation (e.g., 0.6 means you aim to use 60% of maximum lift). Higher values are riskier.

Drone Payload Capacity

— kg
kg Total Takeoff Weight

This is the estimated maximum weight your drone can lift, accounting for its own weight, battery, and a safety margin.

Total Max Thrust

Required Thrust

Effective Payload

Payload vs. Total Weight

Total Takeoff Weight Payload Capacity

Drone Weight Components

Breakdown of Drone Weight
Component Weight (kg) Percentage of Total Weight
Drone Empty Weight –%
Battery Weight –%
Payload Weight –%
Total Takeoff Weight 100%

What is Drone Payload Capacity?

Drone payload capacity refers to the maximum amount of weight that a specific unmanned aerial vehicle (UAV), commonly known as a drone, can safely carry in addition to its own operational weight. This capacity is a critical specification for anyone considering a drone for commercial, industrial, or even advanced hobbyist applications. It dictates the types of equipment, sensors, cameras, or delivery items a drone can transport, directly impacting its usability and effectiveness for a given task.

Who should use it? Anyone operating or purchasing drones for tasks such as aerial photography and videography (carrying heavier cameras), surveying and mapping (transporting specialized sensors), agricultural monitoring (deploying sensors or spraying equipment), infrastructure inspection (carrying thermal or high-resolution cameras), package delivery, or search and rescue operations will benefit from understanding their drone's payload capacity.

Common misconceptions often involve assuming a drone can lift significantly more than its rated capacity, especially in ideal conditions. Many believe that simply adding more powerful motors will indefinitely increase payload, ignoring other critical factors like flight controller limits, airframe integrity, battery life, and flight stability. Furthermore, payload capacity isn't just about lifting; it's about lifting *safely and efficiently* for a reasonable duration and with adequate control.

Drone Payload Capacity Formula and Mathematical Explanation

Calculating a drone's theoretical maximum payload involves understanding the forces at play: thrust generated by the motors versus the total weight to be lifted. A fundamental principle is that for a drone to fly, the total upward thrust must exceed the total downward force (weight).

The core calculation for maximum payload involves determining the total maximum thrust the drone's motors can produce and then subtracting the drone's own weight (including battery and any fixed equipment) from this thrust. A safety factor is then applied to ensure the drone operates within its stable limits.

Step-by-Step Derivation

  1. Calculate Total Maximum Thrust: This is the sum of the maximum thrust each individual motor can generate.
  2. Determine Total Drone Weight: This includes the drone's empty weight plus the weight of the battery.
  3. Calculate Available Thrust for Payload: Subtract the Total Drone Weight from the Total Maximum Thrust. This gives you the theoretical maximum weight the drone *could* lift.
  4. Apply Safety Factor: Multiply the available thrust by a safety factor to determine the practical, safe maximum payload. This accounts for variable conditions, control authority, and preventing motor strain.

Variable Explanations

The key variables used in the calculation are:

Variable Meaning Unit Typical Range
Drone Empty Weight The weight of the drone frame, motors, ESCs, flight controller, etc., without battery or payload. kg 0.5 kg – 30+ kg
Battery Weight The weight of the drone's power source. kg 0.1 kg – 5+ kg
Max Thrust Per Motor The maximum downward force one motor can produce. Often measured in gram-force (gf) or kilogram-force (kgf). We use kgf here for consistency. kgf 0.5 kgf – 10+ kgf
Number of Motors The total count of propulsion units on the drone. Count 4, 6, 8
Total Max Thrust The combined maximum thrust from all motors. kgf Calculated
Required Thrust (for hover) The thrust needed to counteract the total weight of the drone + battery + payload. For stable flight, this should be equal to Total Takeoff Weight. kgf Calculated
Safety Factor A multiplier to ensure the drone operates below its absolute thrust limit for stability and control. Decimal 0.5 – 0.8 (Recommended)
Max Payload Capacity The maximum additional weight the drone can lift safely. kg Calculated
Total Takeoff Weight The combined weight of the drone, battery, and maximum payload. kg Calculated

The Formula

The calculation performed by this calculator is:

Total Max Thrust = Max Thrust Per Motor * Number of Motors

Required Thrust = Drone Empty Weight + Battery Weight + Payload Weight

Theoretical Max Lift = Total Max Thrust

Safe Max Payload = (Theoretical Max Lift - (Drone Empty Weight + Battery Weight)) * Safety Factor

Total Takeoff Weight = Drone Empty Weight + Battery Weight + Safe Max Payload

The calculator ensures that the Total Takeoff Weight does not exceed the Total Max Thrust, and that the Safe Max Payload is what's practically achievable with the chosen safety factor.

Practical Examples (Real-World Use Cases)

Understanding drone payload capacity is crucial for mission planning. Here are a couple of examples:

Example 1: Professional Aerial Photography Drone

Scenario: A photographer is using a quadcopter for high-quality cinematic shots. They need to carry a professional mirrorless camera with a lens.

  • Drone Empty Weight: 4.0 kg
  • Battery Weight: 1.2 kg
  • Max Thrust Per Motor: 3.0 kgf
  • Number of Motors: 4
  • Safety Factor: 0.6 (60%)

Calculation Breakdown:

  • Total Max Thrust = 3.0 kgf * 4 = 12.0 kgf
  • Drone + Battery Weight = 4.0 kg + 1.2 kg = 5.2 kg
  • Theoretical Lift Capacity = 12.0 kg
  • Available Thrust for Payload = 12.0 kg – 5.2 kg = 6.8 kg
  • Safe Max Payload = 6.8 kg * 0.6 = 4.08 kg
  • Total Takeoff Weight = 5.2 kg (drone+battery) + 4.08 kg (payload) = 9.28 kg

Interpretation: This drone can safely carry approximately 4.08 kg of payload. The photographer can use a camera system weighing up to this amount. The total takeoff weight will be around 9.28 kg, which is well below the 12.0 kg total thrust limit.

Example 2: Industrial Inspection Drone

Scenario: An inspection company uses a heavier-lift octocopter equipped with a thermal imaging camera and other sensors for bridge inspections.

  • Drone Empty Weight: 15.0 kg
  • Battery Weight: 3.5 kg
  • Max Thrust Per Motor: 5.5 kgf
  • Number of Motors: 8
  • Safety Factor: 0.55 (55%)

Calculation Breakdown:

  • Total Max Thrust = 5.5 kgf * 8 = 44.0 kgf
  • Drone + Battery Weight = 15.0 kg + 3.5 kg = 18.5 kg
  • Theoretical Lift Capacity = 44.0 kg
  • Available Thrust for Payload = 44.0 kg – 18.5 kg = 25.5 kg
  • Safe Max Payload = 25.5 kg * 0.55 = 14.025 kg
  • Total Takeoff Weight = 18.5 kg (drone+battery) + 14.025 kg (payload) = 32.525 kg

Interpretation: This heavy-lift drone can safely carry approximately 14.03 kg of payload. This allows for significant sensor packages, making it suitable for demanding industrial inspection tasks. The total takeoff weight of ~32.5 kg is comfortably within the 44.0 kg thrust limit.

How to Use This Drone Payload Calculator

Our calculator is designed for simplicity and accuracy. Follow these steps to determine your drone's carrying capacity:

  1. Input Drone Empty Weight: Enter the weight of your drone without the battery or any added equipment.
  2. Input Battery Weight: Enter the weight of the battery you typically use.
  3. Input Max Thrust Per Motor: Find this specification from your drone's manufacturer or motor specifications. Ensure it's in kgf (kilogram-force).
  4. Select Number of Motors: Choose the configuration of your drone (quadcopter, hexacopter, octocopter).
  5. Set Safety Factor: Adjust the safety factor. A value between 0.5 and 0.7 is generally recommended for most applications. Lower values mean less payload but greater stability and safety margin; higher values increase potential payload but reduce safety.
  6. Click 'Calculate Payload': The calculator will instantly display the results.

How to Read Results

  • Max Payload Capacity: This is the primary result – the maximum weight your drone can safely carry.
  • Total Takeoff Weight: The sum of the drone's weight, battery weight, and the calculated maximum payload.
  • Intermediate Values: Total Max Thrust, Required Thrust, and Effective Payload provide insights into the underlying calculations.
  • Weight Components Table: Shows a breakdown of weights and their percentages, helping you visualize the balance.
  • Chart: Visually represents how the total takeoff weight increases with payload, and how it relates to the drone's total thrust capability.

Decision-Making Guidance

Use the results to make informed decisions:

  • Equipment Selection: Ensure your chosen camera, sensors, or delivery items do not exceed the calculated Max Payload Capacity.
  • Safety Assessment: If your required payload is close to the maximum, consider reducing the safety factor (at higher risk) or choosing a drone with a higher thrust capability.
  • Flight Planning: Be aware that carrying maximum payload significantly impacts flight time and maneuverability. Always test with lighter loads first.
  • Drone Upgrades: If you consistently need to carry more weight, you might need a larger drone, more powerful motors, or a different configuration (e.g., upgrading from a quadcopter to a hexacopter).

Key Factors That Affect Drone Payload Results

While the calculator provides a theoretical maximum, several real-world factors can influence how much weight a drone can *actually* carry safely and effectively:

  1. Propeller Efficiency and Size: Larger, more efficient propellers can generate more thrust with less power, effectively increasing payload capacity or flight time. The pitch and diameter are crucial.
  2. Motor KV Rating: The KV rating (RPM per volt) of motors affects their power output and efficiency. Lower KV motors with larger propellers are often better suited for lifting heavier payloads.
  3. Battery Voltage and Discharge Rate (C-Rating): Higher voltage batteries (e.g., 6S vs 4S) and batteries with high C-ratings can deliver more power to the motors, boosting thrust and allowing for heavier payloads.
  4. Air Density (Altitude and Temperature): At higher altitudes or in warmer temperatures, the air is less dense. This reduces propeller efficiency, meaning motors must work harder to generate the same thrust, thereby decreasing effective payload capacity.
  5. Aerodynamic Drag: Adding bulky equipment or operating in windy conditions increases air resistance (drag). This requires more thrust to maintain speed and position, reducing the power available for lifting payload.
  6. Flight Controller Tuning: A well-tuned flight controller is essential for stability. Aggressive tuning might allow slightly more payload but can compromise stability, while conservative tuning ensures smoother flight but might limit maximum lift.
  7. Frame Strength and Rigidity: The drone's airframe must be strong enough to handle the vibrations and stresses of flight, especially when carrying significant weight. A flexible frame can lead to instability.
  8. Power Distribution System: The Electronic Speed Controllers (ESCs) and wiring must be capable of handling the high current draw required for maximum thrust, especially with heavy payloads.

Frequently Asked Questions (FAQ)

What is the difference between 'Max Payload Capacity' and 'Total Takeoff Weight'?
Max Payload Capacity is the *additional* weight the drone can carry (e.g., camera, sensors). Total Takeoff Weight is the *combined* weight of the drone itself, its battery, and the payload.
Why is a Safety Factor important?
A safety factor (e.g., 0.6) ensures the drone operates well below its absolute maximum thrust limit. This provides stability, allows for quick maneuvers (like ascent or obstacle avoidance), prevents motor overheating, and extends component lifespan.
Can I always carry the calculated maximum payload?
The calculator provides a theoretical maximum under ideal conditions. Actual performance may vary due to factors like battery health, wind, temperature, and pilot skill. It's always best to test incrementally.
How does payload affect flight time?
Carrying a heavier payload requires motors to work harder, consuming more power from the battery. This significantly reduces the drone's flight time. The heavier the payload, the shorter the flight.
What happens if I exceed my drone's payload capacity?
Exceeding payload capacity can lead to unstable flight, reduced maneuverability, inability to take off, motor failure, battery strain, or even a crash. It is dangerous and can damage the drone.
Are there specific drones designed for heavy payloads?
Yes, many drones are specifically designed as 'heavy-lift' platforms. These typically have larger frames, more powerful motors, larger propellers, and higher voltage battery systems to achieve significantly higher payload capacities compared to standard consumer or prosumer drones.
How do I find the 'Max Thrust Per Motor' specification?
This information is usually found in the technical specifications provided by the drone manufacturer or the manufacturer of the individual motors and propellers. It might be listed in Newtons (N), which can be converted to kgf (1 kgf ≈ 9.81 N).
Can I modify my drone to increase its payload capacity?
While upgrades like more powerful motors or larger propellers are possible, they require careful consideration of compatibility, power requirements (battery, ESCs), frame strength, and flight controller tuning. It's a complex process that can void warranties and requires significant technical expertise.

Related Tools and Internal Resources

© 2023 YourDroneExperts. All rights reserved.

var chartInstance = null; // Global variable to hold chart instance function calculatePayload() { var droneWeight = parseFloat(document.getElementById("droneWeight").value); var batteryWeight = parseFloat(document.getElementById("batteryWeight").value); var maxThrustPerMotor = parseFloat(document.getElementById("maxThrustPerMotor").value); var numberOfMotors = parseInt(document.getElementById("numberOfMotors").value); var safetyFactor = parseFloat(document.getElementById("safetyFactor").value); var isValid = true; // — Input Validation — if (isNaN(droneWeight) || droneWeight <= 0) { document.getElementById("droneWeightError").innerText = "Please enter a valid drone weight (positive number)."; document.getElementById("droneWeightError").classList.add("visible"); isValid = false; } else { document.getElementById("droneWeightError").innerText = ""; document.getElementById("droneWeightError").classList.remove("visible"); } if (isNaN(batteryWeight) || batteryWeight <= 0) { document.getElementById("batteryWeightError").innerText = "Please enter a valid battery weight (positive number)."; document.getElementById("batteryWeightError").classList.add("visible"); isValid = false; } else { document.getElementById("batteryWeightError").innerText = ""; document.getElementById("batteryWeightError").classList.remove("visible"); } if (isNaN(maxThrustPerMotor) || maxThrustPerMotor <= 0) { document.getElementById("maxThrustPerMotorError").innerText = "Please enter a valid thrust value (positive number)."; document.getElementById("maxThrustPerMotorError").classList.add("visible"); isValid = false; } else { document.getElementById("maxThrustPerMotorError").innerText = ""; document.getElementById("maxThrustPerMotorError").classList.remove("visible"); } if (isNaN(safetyFactor) || safetyFactor 1) { document.getElementById("safetyFactorError").innerText = "Please enter a safety factor between 0.01 and 1."; document.getElementById("safetyFactorError").classList.add("visible"); isValid = false; } else { document.getElementById("safetyFactorError").innerText = ""; document.getElementById("safetyFactorError").classList.remove("visible"); } if (!isValid) { clearResults(); return; } // — Calculations — var totalMaxThrust = maxThrustPerMotor * numberOfMotors; var droneAndBatteryWeight = droneWeight + batteryWeight; var requiredThrustForHover = droneAndBatteryWeight; // Base required thrust without payload // Theoretical max payload is when total thrust equals total weight // Total Weight = Drone + Battery + Payload // Total Thrust = Drone + Battery + Payload => Payload = Total Thrust – Drone – Battery var theoreticalMaxPayload = totalMaxThrust – droneAndBatteryWeight; // Ensure theoretical max payload is not negative if (theoreticalMaxPayload < 0) { theoreticalMaxPayload = 0; } // Apply safety factor to the theoretical max payload var safeMaxPayload = theoreticalMaxPayload * safetyFactor; // Ensure safeMaxPayload is not negative if (safeMaxPayload < 0) { safeMaxPayload = 0; } var totalTakeoffWeight = droneWeight + batteryWeight + safeMaxPayload; // — Update Results Display — document.getElementById("maxPayloadResult").innerText = safeMaxPayload.toFixed(2) + " kg"; document.getElementById("takeoffWeight").innerText = totalTakeoffWeight.toFixed(2); document.getElementById("totalMaxThrust").innerText = totalMaxThrust.toFixed(2); document.getElementById("requiredThrust").innerText = requiredThrustForHover.toFixed(2); // This is the thrust needed just for drone+battery document.getElementById("effectivePayload").innerText = safeMaxPayload.toFixed(2); // — Update Table — document.getElementById("tableDroneWeight").innerText = droneWeight.toFixed(2); document.getElementById("tableBatteryWeight").innerText = batteryWeight.toFixed(2); document.getElementById("tablePayloadWeight").innerText = safeMaxPayload.toFixed(2); document.getElementById("tableTotalWeight").innerText = totalTakeoffWeight.toFixed(2); var percDroneWeight = (droneWeight / totalTakeoffWeight) * 100; var percBatteryWeight = (batteryWeight / totalTakeoffWeight) * 100; var percPayloadWeight = (safeMaxPayload / totalTakeoffWeight) * 100; document.getElementById("percDroneWeight").innerText = percDroneWeight.toFixed(1) + "%"; document.getElementById("percBatteryWeight").innerText = percBatteryWeight.toFixed(1) + "%"; document.getElementById("percPayloadWeight").innerText = percPayloadWeight.toFixed(1) + "%"; // — Update Chart — updateChart(totalMaxThrust, totalTakeoffWeight, safeMaxPayload); } function clearResults() { document.getElementById("maxPayloadResult").innerText = "– kg"; document.getElementById("takeoffWeight").innerText = "–"; document.getElementById("totalMaxThrust").innerText = "–"; document.getElementById("requiredThrust").innerText = "–"; document.getElementById("effectivePayload").innerText = "–"; document.getElementById("tableDroneWeight").innerText = "–"; document.getElementById("tableBatteryWeight").innerText = "–"; document.getElementById("tablePayloadWeight").innerText = "–"; document.getElementById("tableTotalWeight").innerText = "–"; document.getElementById("percDroneWeight").innerText = "–%"; document.getElementById("percBatteryWeight").innerText = "–%"; document.getElementById("percPayloadWeight").innerText = "–%"; if (chartInstance) { chartInstance.destroy(); chartInstance = null; } var ctx = document.getElementById("payloadChart").getContext("2d"); ctx.clearRect(0, 0, ctx.canvas.width, ctx.canvas.height); // Clear canvas if no chart is drawn } function resetForm() { document.getElementById("droneWeight").value = "5.0"; document.getElementById("batteryWeight").value = "1.5"; document.getElementById("maxThrustPerMotor").value = "2.5"; document.getElementById("numberOfMotors").value = "4"; document.getElementById("safetyFactor").value = "0.6"; // Clear errors var errorElements = document.getElementsByClassName("error-message"); for (var i = 0; i < errorElements.length; i++) { errorElements[i].innerText = ""; errorElements[i].classList.remove("visible"); } calculatePayload(); } function copyResults() { var maxPayload = document.getElementById("maxPayloadResult").innerText; var totalWeight = document.getElementById("takeoffWeight").innerText; var totalMaxThrust = document.getElementById("totalMaxThrust").innerText; var requiredThrust = document.getElementById("requiredThrust").innerText; var effectivePayload = document.getElementById("effectivePayload").innerText; var droneWeight = document.getElementById("droneWeight").value; var batteryWeight = document.getElementById("batteryWeight").value; var maxThrustPerMotor = document.getElementById("maxThrustPerMotor").value; var numberOfMotors = document.getElementById("numberOfMotors").value; var safetyFactor = document.getElementById("safetyFactor").value; var resultsText = "— Drone Payload Calculation Results —\n\n"; resultsText += "Maximum Payload Capacity: " + maxPayload + "\n"; resultsText += "Total Takeoff Weight: " + totalWeight + " kg\n\n"; resultsText += "— Key Calculations —\n"; resultsText += "Total Max Thrust: " + totalMaxThrust + " kgf\n"; resultsText += "Required Thrust (Drone + Battery): " + requiredThrust + " kgf\n"; resultsText += "Effective Payload (with Safety Factor): " + effectivePayload + " kg\n\n"; resultsText += "— Input Assumptions —\n"; resultsText += "Drone Empty Weight: " + droneWeight + " kg\n"; resultsText += "Battery Weight: " + batteryWeight + " kg\n"; resultsText += "Max Thrust Per Motor: " + maxThrustPerMotor + " kgf\n"; resultsText += "Number of Motors: " + numberOfMotors + "\n"; resultsText += "Safety Factor: " + safetyFactor + "\n"; // Use a temporary textarea to copy text var tempTextarea = document.createElement("textarea"); tempTextarea.value = resultsText; tempTextarea.style.position = "absolute"; tempTextarea.style.left = "-9999px"; document.body.appendChild(tempTextarea); tempTextarea.select(); try { var successful = document.execCommand('copy'); var msg = successful ? 'Results copied!' : 'Copy failed!'; // Optionally show a temporary message to the user alert(msg); } catch (err) { console.error('Fallback: Oops, unable to copy', err); alert('Copying failed. Please manually select and copy the results.'); } document.body.removeChild(tempTextarea); } function updateChart(totalMaxThrust, currentTotalTakeoffWeight, currentPayload) { var ctx = document.getElementById("payloadChart").getContext("2d"); // Destroy previous chart instance if it exists if (chartInstance) { chartInstance.destroy(); } // Define data points for the chart. We'll show the current state and a potential max. // Let's create a range of payloads to visualize the line. var maxPossiblePayload = Math.max(0, totalMaxThrust – parseFloat(document.getElementById("droneWeight").value) – parseFloat(document.getElementById("batteryWeight").value)); var maxPossibleTakeoffWeight = parseFloat(document.getElementById("droneWeight").value) + parseFloat(document.getElementById("batteryWeight").value) + maxPossiblePayload; var chartDataPoints = []; var payloadStep = Math.max(1, maxPossiblePayload / 10); // Adjust step for smoother or coarser line for (var p = 0; p <= maxPossiblePayload + payloadStep; p += payloadStep) { var takeoffWeight = parseFloat(document.getElementById("droneWeight").value) + parseFloat(document.getElementById("batteryWeight").value) + p; chartDataPoints.push({ payload: p, takeoffWeight: takeoffWeight }); } // Ensure the current calculated state is represented, even if not perfectly on the line steps var currentDroneWeight = parseFloat(document.getElementById("droneWeight").value); var currentBatteryWeight = parseFloat(document.getElementById("batteryWeight").value); var currentSafePayload = parseFloat(document.getElementById("effectivePayload").innerText); var currentTotalTakeoff = currentDroneWeight + currentBatteryWeight + currentSafePayload; // Add current calculated point if it's not already there var foundCurrentPoint = chartDataPoints.some(function(point) { return Math.abs(point.payload – currentSafePayload) = 0) { chartDataPoints.push({ payload: currentSafePayload, takeoffWeight: currentTotalTakeoff }); } // Sort points by payload for the line chart chartDataPoints.sort(function(a, b) { return a.payload – b.payload; }); // Extract data for chart var chartPayloads = chartDataPoints.map(function(point) { return point.payload; }); var chartTakeoffWeights = chartDataPoints.map(function(point) { return point.takeoffWeight; }); chartInstance = new Chart(ctx, { type: 'line', data: { labels: chartPayloads.map(function(p) { return p.toFixed(1); }), // Use payload as labels datasets: [ { label: 'Total Takeoff Weight', data: chartTakeoffWeights, borderColor: '#004a99', // Primary color backgroundColor: 'rgba(0, 74, 153, 0.2)', fill: false, tension: 0.1, pointRadius: 4, pointBackgroundColor: '#004a99' }, { label: 'Max Thrust Limit', data: chartPayloads.map(function() { return totalMaxThrust; }), // Constant line at max thrust borderColor: '#dc3545', // Error color for limit backgroundColor: 'rgba(220, 53, 69, 0.2)', fill: false, borderDash: [5, 5], // Dashed line tension: 0, pointRadius: 0 } ] }, options: { responsive: true, maintainAspectRatio: false, scales: { x: { title: { display: true, text: 'Payload Weight (kg)' }, ticks: { autoSkip: true, maxTicksLimit: 8 } }, y: { title: { display: true, text: 'Weight / Thrust (kg)' }, beginAtZero: true, suggestedMax: Math.max(totalMaxThrust, maxPossibleTakeoffWeight) * 1.1 // Adjust upper limit } }, plugins: { tooltip: { callbacks: { title: function(tooltipItems) { return 'Payload: ' + tooltipItems[0].label + ' kg'; }, label: function(context) { var label = context.dataset.label || "; if (label) { label += ': '; } if (context.parsed.y !== null) { label += context.parsed.y.toFixed(2) + ' kg'; } return label; } } }, legend: { display: false // Use custom legend } } } }); } // Initialize chart with default values on load window.onload = function() { calculatePayload(); }; <!– –>

Leave a Comment