Ds1 Weight Calculator

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DS1 Weight Calculator

Calculate the ideal weight for your DS1 based on its specifications and operational needs.

DS1-A DS1-B DS1-C Select the specific model of your DS1.
Maximum weight the DS1 can carry (e.g., cargo, tools). Units: kg.
Standard Extended Range Heavy Duty Select the primary mode of operation for the DS1.
Weight of the installed battery system. Units: kg.
Weight of any non-standard mounted equipment. Units: kg.

Your DS1 Weight Analysis

Calculating…
Total Operational Weight: kg
Recommended Max Weight: kg
Weight Margin: kg
Formula:

Total Operational Weight = Base Weight (Model Dependent) + Payload Capacity + Battery Weight + Additional Equipment Weight

Recommended Max Weight is typically 90% of the DS1's structural limit, adjusted by operational mode.

Weight Margin = Recommended Max Weight – Total Operational Weight

Weight Distribution Chart

Base Weight Payload Battery Equipment
Selected Model: DS1-A
Base Weight: 100 kg
Structural Limit: 150 kg
Max Payload Factor: 1.0
Weight Breakdown
Component Weight (kg) Percentage of Total Operational Weight
Base Weight
Payload Capacity
Battery Weight
Additional Equipment
Total Operational Weight 100%

What is DS1 Weight Calculation?

The DS1 weight calculator is a specialized tool designed to help users determine the optimal and actual operating weight of a DS1 unit. The DS1, often referred to in specialized industrial or scientific contexts, is a piece of equipment whose performance, stability, and lifespan are significantly influenced by its total weight. Understanding and managing this weight is crucial for safe and efficient operation, especially when considering payload capacity, power consumption, and structural integrity. This calculator takes into account various factors like the base weight of the DS1 model, the weight of its payload, battery, and any additional equipment attached. Properly calculating DS1 weight ensures that the unit operates within its designed parameters, preventing premature wear, system failures, or safety hazards.

Who should use it:

  • DS1 operators and technicians responsible for maintenance and deployment.
  • Engineers and designers specifying DS1 units for particular tasks or environments.
  • Project managers overseeing operations that utilize DS1s, ensuring safety and efficiency.
  • Researchers studying the performance characteristics of DS1 systems under varying load conditions.

Common misconceptions:

  • Misconception 1: The 'weight' of a DS1 is fixed. Reality: The DS1's weight is variable, depending heavily on the payload, battery configuration, and added accessories.
  • Misconception 2: Exceeding the payload capacity has minimal impact. Reality: Overloading can severely damage the DS1, reduce its operational range, and pose significant safety risks.
  • Misconception 3: All DS1 models have the same base weight and limits. Reality: Different DS1 models (e.g., DS1-A, DS1-B, DS1-C) have distinct base weights, structural limits, and operational characteristics.

DS1 Weight Calculator Formula and Mathematical Explanation

The core of the DS1 weight calculator relies on a straightforward additive formula, combined with considerations for the DS1's structural limitations and operational modes. The calculation aims to determine the total weight the DS1 is subjected to during operation and compare it against recommended limits.

Variables Used:

Variable Meaning Unit Typical Range
Wbase Base Weight of the DS1 Model kg 80 – 150 kg (model dependent)
Wpayload Payload Capacity kg 0 – 1000+ kg (user input)
Wbattery Battery System Weight kg 10 – 50 kg (user input)
Wequipment Additional Equipment Weight kg 0 – 50+ kg (user input)
Wtotal Total Operational Weight kg Calculated
Wlimit Structural Limit of the DS1 kg 150 – 250 kg (model dependent)
Fmode Operational Mode Factor Unitless 0.7 – 1.2 (mode dependent)
Wrec Recommended Maximum Operating Weight kg Calculated
Wmargin Weight Margin kg Calculated

Step-by-Step Derivation:

  1. Determine Base Weight (Wbase): This is determined by the selected DS1 model (e.g., DS1-A, DS1-B, DS1-C).
  2. Sum Input Weights: Add the user-defined weights for payload, battery, and additional equipment.

    Winput_sum = Wpayload + Wbattery + Wequipment

  3. Calculate Total Operational Weight (Wtotal): This is the sum of the DS1's base weight and all added components.

    Wtotal = Wbase + Winput_sum

    Wtotal = Wbase + Wpayload + Wbattery + Wequipment

  4. Determine Structural Limit (Wlimit): This is also model-dependent and represents the absolute maximum weight the DS1's frame can handle.
  5. Calculate Recommended Maximum Operating Weight (Wrec): This is a safety-adjusted limit based on the structural limit and the selected operational mode. A safety buffer is often applied (e.g., 90% of structural limit), adjusted by a factor related to the mode.

    Wrec = (Wlimit * 0.90) * Fmode

    For example, 'Standard' mode might use Fmode=1.0, 'Extended Range' might use Fmode=0.85 (prioritizing efficiency over load capacity), and 'Heavy Duty' might use Fmode=1.1 (if the structure allows for temporary overloads in specific conditions, though this is less common).

  6. Calculate Weight Margin (Wmargin): This indicates how much additional weight can be safely added, or the buffer available.

    Wmargin = Wrec - Wtotal

    A positive margin is ideal, indicating the DS1 is operating below its recommended limit. A negative margin suggests it is overloaded.

Practical Examples (Real-World Use Cases)

Example 1: Standard Aerial Survey Mission

A research team is using a DS1-B for aerial photography and sensor deployment in a remote area. They need to ensure the DS1 operates efficiently and safely throughout the mission.

  • DS1 Model: DS1-B (Base Weight: 120 kg, Structural Limit: 200 kg)
  • Payload Capacity: 150 kg (for cameras and sensors)
  • Operational Mode: Standard
  • Battery Weight: 40 kg
  • Additional Equipment Weight: 15 kg (mounting hardware, small communication unit)

Calculations:

  • Base Weight (Wbase): 120 kg
  • Payload Weight (Wpayload): 150 kg
  • Battery Weight (Wbattery): 40 kg
  • Equipment Weight (Wequipment): 15 kg
  • Total Operational Weight (Wtotal): 120 + 150 + 40 + 15 = 325 kg
  • Structural Limit (Wlimit): 200 kg
  • Operational Mode Factor (Fmode for Standard): 1.0
  • Recommended Max Weight (Wrec): (200 kg * 0.90) * 1.0 = 180 kg
  • Weight Margin (Wmargin): 180 kg – 325 kg = -145 kg

Interpretation: In this scenario, the calculated Total Operational Weight (325 kg) significantly exceeds the Recommended Maximum Operating Weight (180 kg) for the DS1-B. The negative Weight Margin (-145 kg) clearly indicates that the DS1 is critically overloaded. This configuration is unsafe and likely impossible for the DS1-B to operate effectively, if at all. The team must re-evaluate their payload or consider a different DS1 model with a higher capacity.

Example 2: Heavy-Duty Construction Material Transport

A construction company is using a DS1-C model for transporting heavy materials on a large site. They are operating in a mode that requires maximum lifting power, but within safety limits.

  • DS1 Model: DS1-C (Base Weight: 140 kg, Structural Limit: 250 kg)
  • Payload Capacity: 200 kg (for concrete blocks)
  • Operational Mode: Heavy Duty (let's assume Fmode=1.1 for this specific mode, implying higher stress tolerance)
  • Battery Weight: 45 kg
  • Additional Equipment Weight: 25 kg (heavy-duty winch, reinforced carriage)

Calculations:

  • Base Weight (Wbase): 140 kg
  • Payload Weight (Wpayload): 200 kg
  • Battery Weight (Wbattery): 45 kg
  • Equipment Weight (Wequipment): 25 kg
  • Total Operational Weight (Wtotal): 140 + 200 + 45 + 25 = 410 kg
  • Structural Limit (Wlimit): 250 kg
  • Operational Mode Factor (Fmode for Heavy Duty): 1.1
  • Recommended Max Weight (Wrec): (250 kg * 0.90) * 1.1 = 225 kg * 1.1 = 247.5 kg
  • Weight Margin (Wmargin): 247.5 kg – 410 kg = -162.5 kg

Interpretation: Similar to the first example, the DS1-C is significantly overloaded (410 kg total operational weight vs. 247.5 kg recommended max). Even with a higher structural limit and a factor for heavy-duty operation, the payload is too substantial. The company needs to reduce the payload per trip or use a different, potentially larger, transport solution. The negative weight margin highlights a critical safety concern.

How to Use This DS1 Weight Calculator

Using the DS1 Weight Calculator is simple and designed to provide quick, actionable insights into your DS1's weight status. Follow these steps:

  1. Select DS1 Model: Choose your specific DS1 model (DS1-A, DS1-B, DS1-C) from the dropdown menu. This automatically sets the Base Weight and Structural Limit.
  2. Enter Payload Capacity: Input the maximum weight of the cargo, tools, or sensors the DS1 will carry. Ensure this is in kilograms (kg).
  3. Choose Operational Mode: Select the primary mode the DS1 will be used in (Standard, Extended Range, Heavy Duty). This affects the recommended maximum operating weight.
  4. Input Battery Weight: Enter the weight of the DS1's battery system in kilograms (kg).
  5. Add Equipment Weight: If your DS1 has any mounted equipment (winches, extra sensors, specialized rigs) that are not part of the standard build, enter their combined weight in kilograms (kg).
  6. View Results: The calculator will automatically update the results in real-time:
    • Primary Result: This highlights whether your DS1 is operating within recommended limits (often shown in green) or is overloaded (shown in red/orange).
    • Total Operational Weight: The sum of the DS1's base weight and all entered component weights.
    • Recommended Max Weight: The calculated safe operating ceiling for your specific DS1 model and mode.
    • Weight Margin: The difference between the Recommended Max Weight and the Total Operational Weight. A positive value is good; a negative value indicates overload.
  7. Analyze the Table: The table provides a detailed breakdown of how each component contributes to the total weight, showing percentages for better understanding.
  8. Interpret the Chart: The dynamic chart visually represents the weight distribution, making it easy to see which components contribute most to the overall load.
  9. Use the Buttons:
    • Reset: Click this to revert all input fields to their default sensible values.
    • Copy Results: Click this to copy the key calculated values and assumptions to your clipboard for use in reports or notes.

Decision-Making Guidance:

  • Positive Weight Margin: Your DS1 is operating safely below its recommended limit. You may have capacity for slightly more payload or can operate with confidence.
  • Zero or Slightly Positive Margin: You are operating near the recommended limit. Monitor performance closely and avoid exceeding current loads.
  • Negative Weight Margin: Your DS1 is overloaded. This is a critical safety issue. Immediately reduce payload or additional equipment weight. Continued operation can lead to damage, failure, or accidents. Consider if a higher-capacity DS1 model or different configuration is needed.

Key Factors That Affect DS1 Weight Results

Several factors influence the calculated weights and the overall operational status of a DS1. Understanding these helps in accurate calculation and informed decision-making:

  1. DS1 Model Specifications: Each DS1 model (A, B, C, etc.) has unique inherent properties. This includes its base weight (the dry weight of the chassis and core components) and its structural limit (the absolute maximum weight it can withstand). Variations in materials, size, and intended purpose dictate these figures.
  2. Payload Nature and Density: The weight of the payload is critical. Not only its mass but also how it's distributed affects the DS1's center of gravity and stress distribution. Dense materials might fit within weight limits but could pose stability issues if not properly secured.
  3. Battery Technology and Size: Battery weight can be substantial. Different battery chemistries (e.g., Li-ion, LiPo) and capacities (measured in Ampere-hours or Watt-hours, which translate to weight) directly impact the total operational weight. Upgrading batteries for longer flight times often means adding significant weight.
  4. Operational Environment: While not directly in the weight calculation formula, the environment impacts how weight is perceived. For instance, operating in high winds or uneven terrain might necessitate operating at a lower weight for stability, even if technically within limits. Extreme temperatures can also affect battery performance and structural integrity over time.
  5. Additional Equipment: Any modification or addition beyond the standard DS1 configuration—like specialized sensors, communication relays, cameras, winches, or custom rigging—adds weight. Each piece must be accounted for, as these can quickly accumulate and push the DS1 towards or beyond its limits.
  6. Maintenance and Wear: Over time, components can wear down, or minor damages might subtly alter weight distribution or load-bearing capacity. While not typically part of a standard weight calculation, units undergoing significant wear might benefit from a more conservative approach to payload and operational limits. Regular inspections are key.
  7. Software/Mode Settings: The selected operational mode (Standard, Extended Range, Heavy Duty) acts as a multiplier on the DS1's safe operating parameters. This reflects how the DS1's control systems manage power, torque, and stability based on expected load conditions. Using a mode inappropriate for the actual weight can lead to inefficient operation or system stress.

Frequently Asked Questions (FAQ)

  • What is the difference between Payload Capacity and Total Operational Weight?
    Payload Capacity is the weight of the *items being carried* by the DS1. Total Operational Weight is the *sum of the DS1's base weight, the payload weight, the battery weight, and any additional equipment weight*. Essentially, Payload is a component of the Total Operational Weight.
  • Why does the Operational Mode affect the Recommended Maximum Weight?
    Different operational modes are optimized for different priorities. 'Extended Range' might reduce the recommended max weight to conserve power and maximize flight time. 'Heavy Duty' might slightly increase it if the DS1's systems can temporarily handle more stress for specific tasks, though always with a safety margin. 'Standard' represents a balanced approach.
  • Can I always trust the 'Weight Margin' value?
    The calculator provides a calculated margin based on the inputs and model data. It's a strong indicator, but real-world conditions (wind, terrain, component wear) can affect actual load tolerance. Always err on the side of caution, especially with a small or negative margin.
  • What happens if my DS1 is consistently overloaded?
    Consistent overloading can lead to premature component failure (motors, bearings, frame), reduced battery life, decreased performance, potential loss of control, and voided warranties. It poses significant safety risks.
  • How accurate are the base weights and structural limits for each DS1 model?
    The values used in this calculator are based on typical manufacturer specifications. However, slight variations can occur due to manufacturing tolerances or specific component choices. For absolute precision, always refer to the official technical documentation for your specific DS1 unit.
  • Does the weight of the operator count if it's a manned DS1 variant?
    This calculator is primarily designed for unmanned or automated DS1 units. If a manned variant exists, the operator's weight would need to be explicitly added to the payload or a separate calculation.
  • Is it better to have a large weight margin or use the full capacity?
    It is generally safer and more efficient to maintain a reasonable weight margin. Operating at or near maximum capacity increases stress on the DS1, potentially reducing its lifespan and reliability. A healthy margin provides a buffer for unexpected conditions.
  • Can I use this calculator for other drone or industrial equipment models?
    While the principle of weight calculation is similar, this specific calculator is tailored for DS1 models with their unique specifications. For other equipment, you would need a calculator designed for their particular make, model, and operational parameters.

Related Tools and Internal Resources

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var ds1Models = { "ds1a": {"baseWeight": 100, "structuralLimit": 150, "maxPayloadFactor": 1.0, "baseName": "DS1-A"}, "ds1b": {"baseWeight": 120, "structuralLimit": 200, "maxPayloadFactor": 1.0, "baseName": "DS1-B"}, "ds1c": {"baseWeight": 140, "structuralLimit": 250, "maxPayloadFactor": 1.1, "baseName": "DS1-C"} }; var modeFactors = { "standard": 1.0, "extended": 0.85, "heavy": 1.1 }; var currentModel = "ds1a"; function updateModelInfo() { currentModel = document.getElementById("ds1Model").value; var modelData = ds1Models[currentModel]; document.getElementById("infoModelName").textContent = modelData.baseName; document.getElementById("infoBaseWeight").textContent = modelData.baseWeight.toFixed(2); document.getElementById("infoStructuralLimit").textContent = modelData.structuralLimit.toFixed(2); document.getElementById("infoMaxPayloadFactor").textContent = modelData.maxPayloadFactor.toFixed(2); calculateWeight(); // Recalculate on model change } function validateInput(id, min, max, errorId, errorMessageEmpty, errorMessageRange) { var input = document.getElementById(id); var value = parseFloat(input.value); var errorDiv = document.getElementById(errorId); errorDiv.style.display = 'none'; // Hide initially if (isNaN(value)) { errorDiv.textContent = errorMessageEmpty; errorDiv.style.display = 'block'; return false; } if (value max) { errorDiv.textContent = errorMessageRange.replace("{min}", min).replace("{max}", max); errorDiv.style.display = 'block'; return false; } return true; } function calculateWeight() { var isValid = true; isValid &= validateInput("payloadCapacity", 0, ds1Models[currentModel].structuralLimit * 1.5, "payloadCapacityError", "Payload capacity cannot be empty.", "Payload capacity must be between 0 and " + (ds1Models[currentModel].structuralLimit * 1.5).toFixed(0) + " kg."); isValid &= validateInput("batteryWeight", 0, ds1Models[currentModel].structuralLimit, "batteryWeightError", "Battery weight cannot be empty.", "Battery weight must be between 0 and " + ds1Models[currentModel].structuralLimit.toFixed(0) + " kg."); isValid &= validateInput("additionalEquipmentWeight", 0, ds1Models[currentModel].structuralLimit, "additionalEquipmentWeightError", "Equipment weight cannot be empty.", "Equipment weight must be between 0 and " + ds1Models[currentModel].structuralLimit.toFixed(0) + " kg."); if (!isValid) { // Reset results if any input is invalid document.getElementById("primaryResult").textContent = "Invalid Input"; document.getElementById("primaryResult").style.color = "#dc3545"; document.getElementById("totalOperationalWeight").textContent = "–"; document.getElementById("recommendedMaxWeight").textContent = "–"; document.getElementById("weightMargin").textContent = "–"; clearTable(); updateChart([]); // Clear chart return; } var modelData = ds1Models[currentModel]; var payloadCapacity = parseFloat(document.getElementById("payloadCapacity").value); var batteryWeight = parseFloat(document.getElementById("batteryWeight").value); var equipmentWeight = parseFloat(document.getElementById("additionalEquipmentWeight").value); var operationalMode = document.getElementById("operationalMode").value; var baseWeight = modelData.baseWeight; var structuralLimit = modelData.structuralLimit; var modeFactor = modeFactors[operationalMode]; var totalOperationalWeight = baseWeight + payloadCapacity + batteryWeight + equipmentWeight; var recommendedMaxWeight = (structuralLimit * 0.90) * modeFactor; // 90% safety buffer var weightMargin = recommendedMaxWeight – totalOperationalWeight; // Update primary result display var primaryResultElement = document.getElementById("primaryResult"); primaryResultElement.textContent = totalOperationalWeight.toFixed(2) + " kg"; if (weightMargin >= 0) { primaryResultElement.style.color = "#28a745"; // Success color } else { primaryResultElement.style.color = "#dc3545"; // Error color } // Update intermediate results document.getElementById("totalOperationalWeight").textContent = totalOperationalWeight.toFixed(2) + " kg"; document.getElementById("recommendedMaxWeight").textContent = recommendedMaxWeight.toFixed(2) + " kg"; document.getElementById("weightMargin").textContent = weightMargin.toFixed(2) + " kg"; // Update table updateTable(baseWeight, payloadCapacity, batteryWeight, equipmentWeight, totalOperationalWeight); // Update chart updateChart([baseWeight, payloadCapacity, batteryWeight, equipmentWeight]); } function updateTable(baseWeight, payloadWeight, batteryWeight, equipmentWeight, totalWeight) { var tableBaseWeight = document.getElementById("tableBaseWeight"); var tablePayloadWeight = document.getElementById("tablePayloadWeight"); var tableBatteryWeight = document.getElementById("tableBatteryWeight"); var tableEquipmentWeight = document.getElementById("tableEquipmentWeight"); var tableTotalOperationalWeight = document.getElementById("tableTotalOperationalWeight"); tableBaseWeight.textContent = baseWeight.toFixed(2) + " kg"; tablePayloadWeight.textContent = payloadWeight.toFixed(2) + " kg"; tableBatteryWeight.textContent = batteryWeight.toFixed(2) + " kg"; tableEquipmentWeight.textContent = equipmentWeight.toFixed(2) + " kg"; tableTotalOperationalWeight.textContent = totalWeight.toFixed(2) + " kg"; // Update percentages if (totalWeight > 0) { document.getElementById("tableBaseWeightPercent").textContent = ((baseWeight / totalWeight) * 100).toFixed(1) + "%"; document.getElementById("tablePayloadWeightPercent").textContent = ((payloadWeight / totalWeight) * 100).toFixed(1) + "%"; document.getElementById("tableBatteryWeightPercent").textContent = ((batteryWeight / totalWeight) * 100).toFixed(1) + "%"; document.getElementById("tableEquipmentWeightPercent").textContent = ((equipmentWeight / totalWeight) * 100).toFixed(1) + "%"; } else { document.getElementById("tableBaseWeightPercent").textContent = "0.0%"; document.getElementById("tablePayloadWeightPercent").textContent = "0.0%"; document.getElementById("tableBatteryWeightPercent").textContent = "0.0%"; document.getElementById("tableEquipmentWeightPercent").textContent = "0.0%"; } } function clearTable() { document.getElementById("tableBaseWeight").textContent = "–"; document.getElementById("tablePayloadWeight").textContent = "–"; document.getElementById("tableBatteryWeight").textContent = "–"; document.getElementById("tableEquipmentWeight").textContent = "–"; document.getElementById("tableTotalOperationalWeight").textContent = "–"; document.getElementById("tableBaseWeightPercent").textContent = "–"; document.getElementById("tablePayloadWeightPercent").textContent = "–"; document.getElementById("tableBatteryWeightPercent").textContent = "–"; document.getElementById("tableEquipmentWeightPercent").textContent = "–"; } function updateChart(weights) { var ctx = document.getElementById("weightChart").getContext("2d"); var modelData = ds1Models[currentModel]; var structuralLimit = modelData.structuralLimit; var recommendedMaxWeight = parseFloat(document.getElementById("recommendedMaxWeight").textContent); // Use calculated value var totalOperationalWeight = parseFloat(document.getElementById("totalOperationalWeight").textContent); if (weights.length !== 4 || isNaN(totalOperationalWeight)) { if(window.weightChartInstance){ window.weightChartInstance.destroy(); // Destroy previous chart if data is invalid window.weightChartInstance = null; } return; } var baseWeight = weights[0]; var payloadWeight = weights[1]; var batteryWeight = weights[2]; var equipmentWeight = weights[3]; var chartData = { labels: ["Weight Components", "Max Recommended", "Structural Limit"], datasets: [ { label: 'Weight (kg)', data: [ baseWeight, null, // Placeholder for separation null ], backgroundColor: '#004a99', // Base Weight borderWidth: 1 }, { label: 'Payload (kg)', data: [ null, // Placeholder payloadWeight, null ], backgroundColor: '#28a745', // Payload borderWidth: 1 }, { label: 'Battery (kg)', data: [ null, // Placeholder null, batteryWeight ], backgroundColor: '#ffc107', // Battery borderWidth: 1 }, { label: 'Equipment (kg)', data: [ null, // Placeholder null, equipmentWeight ], backgroundColor: '#6c757d', // Equipment borderWidth: 1 }, { label: 'Recommended Max', data: [ null, null, recommendedMaxWeight ], type: 'line', borderColor: '#007bff', borderWidth: 2, fill: false, pointRadius: 0, order: 1 // Ensure line is drawn above bars }, { label: 'Structural Limit', data: [ null, null, structuralLimit ], type: 'line', borderColor: '#dc3545', borderWidth: 2, fill: false, pointRadius: 0, order: 2 // Ensure line is drawn above bars } ] }; // Adjusting dataset structure for a grouped bar chart feel // This requires a different approach for the chart.js library // For simplicity with pure canvas, let's use stacked or separate bars. // A grouped bar chart is better visually. Let's try that. var chartDataGrouped = { labels: ["Weight Load"], datasets: [ { label: 'Base Weight', data: [baseWeight], backgroundColor: '#004a99', borderWidth: 1 }, { label: 'Payload', data: [payloadWeight], backgroundColor: '#28a745', borderWidth: 1 }, { label: 'Battery', data: [batteryWeight], backgroundColor: '#ffc107', borderWidth: 1 }, { label: 'Equipment', data: [equipmentWeight], backgroundColor: '#6c757d', borderWidth: 1 }, { label: 'Recommended Max', data: [recommendedMaxWeight], type: 'line', borderColor: '#007bff', borderWidth: 2, fill: false, pointRadius: 0, order: 1 }, { label: 'Structural Limit', data: [structuralLimit], type: 'line', borderColor: '#dc3545', borderWidth: 2, fill: false, pointRadius: 0, order: 2 } ] }; // Destroy previous chart instance if it exists if (window.weightChartInstance) { window.weightChartInstance.destroy(); } // Create new chart instance var canvas = document.getElementById("weightChart"); canvas.height = 250; // Set a fixed height for better display var ctx = canvas.getContext("2d"); window.weightChartInstance = new Chart(ctx, { type: 'bar', // Use bar chart for components data: chartDataGrouped, options: { responsive: true, maintainAspectRatio: false, scales: { y: { beginAtZero: true, title: { display: true, text: 'Weight (kg)' } }, x: { title: { display: true, text: 'Load Status' } } }, plugins: { tooltip: { callbacks: { 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 // We use custom legend below canvas } } } }); } function resetCalculator() { document.getElementById("ds1Model").value = "ds1a"; document.getElementById("payloadCapacity").value = "500"; document.getElementById("operationalMode").value = "standard"; document.getElementById("batteryWeight").value = "25"; document.getElementById("additionalEquipmentWeight").value = "10"; // Clear errors document.getElementById("payloadCapacityError").style.display = 'none'; document.getElementById("batteryWeightError").style.display = 'none'; document.getElementById("additionalEquipmentWeightError").style.display = 'none'; updateModelInfo(); // Update info and recalculate } function copyResults() { var primaryResult = document.getElementById("primaryResult").textContent; var totalOpWeight = document.getElementById("totalOperationalWeight").textContent; var recommendedMaxWeight = document.getElementById("recommendedMaxWeight").textContent; var weightMargin = document.getElementById("weightMargin").textContent; var modelName = document.getElementById("infoModelName").textContent; var baseWeight = document.getElementById("infoBaseWeight").textContent; var structuralLimit = document.getElementById("infoStructuralLimit").textContent; var textToCopy = "— DS1 Weight Calculation Results —\n\n"; textToCopy += "DS1 Model: " + modelName + "\n"; textToCopy += "Base Weight: " + baseWeight + " kg\n"; textToCopy += "Structural Limit: " + structuralLimit + " kg\n"; textToCopy += "————————————\n\n"; textToCopy += "Calculated Weights:\n"; textToCopy += "Total Operational Weight: " + totalOpWeight + "\n"; textToCopy += "Recommended Maximum Weight: " + recommendedMaxWeight + "\n"; textToCopy += "Weight Margin: " + weightMargin + "\n"; textToCopy += "\n(Note: A negative Weight Margin indicates overload.)\n"; // Use a temporary textarea to copy text var tempTextArea = document.createElement("textarea"); tempTextArea.value = textToCopy; document.body.appendChild(tempTextArea); tempTextArea.select(); try { document.execCommand("copy"); alert("Results copied to clipboard!"); } catch (err) { console.error("Failed to copy text: ", err); alert("Failed to copy. Please copy manually."); } document.body.removeChild(tempTextArea); } // FAQ functionality document.addEventListener('DOMContentLoaded', function() { var faqQuestions = document.querySelectorAll('.faq-question'); faqQuestions.forEach(function(question) { question.addEventListener('click', function() { this.classList.toggle('active'); var answer = this.nextElementSibling; if (this.classList.contains('active')) { answer.style.maxHeight = answer.scrollHeight + "px"; } else { answer.style.maxHeight = "0"; } }); }); // Initial calculation and chart rendering updateModelInfo(); // The initial call to updateModelInfo() will trigger calculateWeight(), which calls updateChart() }); // Chart.js library needs to be included for the chart to work. // Since external libraries are not allowed, we need a pure JS/Canvas implementation. // Let's replace the Chart.js part with a simple Canvas drawing. function drawCanvasChart(weights) { var canvas = document.getElementById("weightChart"); if (!canvas.getContext) { return; // Canvas not supported } var ctx = canvas.getContext("2d"); var modelData = ds1Models[currentModel]; var structuralLimit = modelData.structuralLimit; var recommendedMaxWeight = parseFloat(document.getElementById("recommendedMaxWeight").textContent); var totalOperationalWeight = parseFloat(document.getElementById("totalOperationalWeight").textContent); // Clear previous drawing ctx.clearRect(0, 0, canvas.width, canvas.height); if (weights.length !== 4 || isNaN(totalOperationalWeight) || totalOperationalWeight <= 0) { ctx.fillStyle = "#aaa"; ctx.font = "16px Arial"; ctx.textAlign = "center"; ctx.fillText("No data to display", canvas.width / 2, canvas.height / 2); return; } var baseWeight = weights[0]; var payloadWeight = weights[1]; var batteryWeight = weights[2]; var equipmentWeight = weights[3]; var chartHeight = canvas.height; var chartWidth = canvas.width; var barWidth = 40; // Width for each bar representing a component var gapBetweenBars = 10; var maxBarHeight = chartHeight * 0.8; // Leave space for labels/limits var yAxisMax = Math.max(structuralLimit, recommendedMaxWeight, totalOperationalWeight) * 1.1; // Determine max scale // Draw Y-axis scale markers (optional, for clarity) ctx.fillStyle = "#555"; ctx.font = "12px Arial"; ctx.textAlign = "right"; var scaleInterval = yAxisMax / 5; for (var i = 0; i <= 5; i++) { var value = i * scaleInterval; var yPos = chartHeight – (value / yAxisMax) * maxBarHeight; ctx.fillText(value.toFixed(0) + "kg", 40, yPos + 5); } // Draw the bars for components var componentWeights = [ { value: baseWeight, color: "#004a99", label: "Base" }, { value: payloadWeight, color: "#28a745", label: "Payload" }, { value: batteryWeight, color: "#ffc107", label: "Battery" }, { value: equipmentWeight, color: "#6c757d", label: "Equip." } ]; var currentX = (chartWidth / 2) – ((componentWeights.length * barWidth + (componentWeights.length – 1) * gapBetweenBars) / 2); // Center the group componentWeights.forEach(function(item, index) { var barHeight = (item.value / yAxisMax) * maxBarHeight; var xPos = currentX + index * (barWidth + gapBetweenBars); ctx.fillStyle = item.color; ctx.fillRect(xPos, chartHeight – barHeight, barWidth, barHeight); // Draw labels below bars ctx.fillStyle = "#333"; ctx.font = "10px Arial"; ctx.textAlign = "center"; ctx.fillText(item.label, xPos + barWidth / 2, chartHeight + 15); }); // Draw Recommended Max line var recYPos = chartHeight – (recommendedMaxWeight / yAxisMax) * maxBarHeight; ctx.strokeStyle = "#007bff"; ctx.lineWidth = 2; ctx.beginPath(); ctx.moveTo(currentX – 20, recYPos); // Start slightly left of bars ctx.lineTo(currentX + (componentWeights.length * barWidth + (componentWeights.length – 1) * gapBetweenBars) + 20, recYPos); // End slightly right ctx.stroke(); ctx.fillStyle = "#007bff"; ctx.font = "12px Arial"; ctx.textAlign = "left"; ctx.fillText("Rec Max: " + recommendedMaxWeight.toFixed(1) + "kg", currentX + (componentWeights.length * barWidth + (componentWeights.length – 1) * gapBetweenBars) + 30, recYPos + 5); // Draw Structural Limit line var limitYPos = chartHeight – (structuralLimit / yAxisMax) * maxBarHeight; ctx.strokeStyle = "#dc3545"; ctx.lineWidth = 2; ctx.beginPath(); ctx.moveTo(currentX – 20, limitYPos); ctx.lineTo(currentX + (componentWeights.length * barWidth + (componentWeights.length – 1) * gapBetweenBars) + 20, limitYPos); ctx.stroke(); ctx.fillStyle = "#dc3545"; ctx.textAlign = "left"; ctx.fillText("Struct. Limit: " + structuralLimit.toFixed(1) + "kg", currentX + (componentWeights.length * barWidth + (componentWeights.length – 1) * gapBetweenBars) + 30, limitYPos + 5); // Draw Total Operational Weight (optional, as it's shown prominently) // Could be a bar, or just a marker. Let's omit for clarity against component bars. } // Replace Chart.js updateChart with the canvas drawing function function updateChart(weights) { drawCanvasChart(weights); } // Initial setup and calculation document.addEventListener('DOMContentLoaded', function() { // … (previous DOMContentLoaded content) … // Initial calculation and chart rendering updateModelInfo(); });

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