Need to input all the following details for a UK Operations Manual, i know some of these details are online which i can fill in, but not all. Do you have a document that answers all of the below?
UAS General DescriptionPlease confirm or provide the following details for the ModalAI PX4:
1.1 Aircraft Identification Make Model Variant / Configuration (if applicable) Type of Aircraft (e.g. multirotor, quadcopter) Serial Number Format Date of Manufacture Intended Operational Category (if defined by manufacturer)
1.2 Aircraft Specifications Official Aircraft Specification Weblink Maximum Take-off Mass (MTOM) (grams) Maximum Payload Mass (grams) Empty Weight (without battery & payload)
1.3 Dimensions
Please confirm all dimensions with propellers installed: Length (mm) Width (mm) Height (mm) Diagonal Motor-to-Motor Distance (mm) (if applicable)
1.4 Propulsion Configuration Propeller Configuration (e.g. quadcopter, X-configuration) Motor Orientation (pusher / puller / mixed) Number of Motors UA Performance Characteristics (Flight Envelope)
Please confirm the following performance limits:
2.1 Mass & Speed Maximum Take-off Mass (MTOM) (g) Maximum Airspeed (m/s or km/h) Minimum Airspeed to Maintain Safe Flight ☐ N/A (multirotor – hover capable) ☐ Value (if applicable)
2.2 Manoeuvring Limits Maximum Bank Angle (degrees) Maximum Pitch Angle (degrees) Maximum Yaw Rate (deg/s or rad/s)
2.3 Altitude & Endurance
Normal Operating Height (AGL) (m) Maximum Operating Height (Service Ceiling) (AMSL, m) Maximum Flight Time (minutes – hover, no wind, standard battery) Maximum Operating Range (km) Maximum Command & Control (C2) Range (km)2.4 Failure & Recovery Glide Distance (if applicable) Failsafe Behaviours (e.g. RTH, land, hover) Loss of GNSS Behaviour Loss of C2 Behaviour
2.5 Other Performance Information Any Additional Performance Limitations or Notes UAS Environmental Limitations
Please confirm environmental operating limits:
3.1 Wind Maximum Wind Speed for Take-off & Landing (steady + gusts, m/s) Maximum Wind Speed for Sustained Flight (steady + gusts, m/s)
3.2 Weather & Exposure Ingress Protection (IP) Rating Precipitation Limitations (rain, drizzle, snow – if any) In-flight Icing Tolerance (Yes / No / N/A)
3.3 Temperature Maximum Operating Air Temperature (°C) Minimum Operating Air Temperature (°C)
3.4 Other Environmental Factors Space Weather / GNSS Interference Limitations Any Other Environmental Restrictions Fuel / Energy Source (General)
4.1 Energy Type Energy Source Type (e.g. batteries) Number of Energy Sources Installed Means of Identifying Energy State (LEDs, app, telemetry) Fuel / Energy Status Indicators Fuel / Energy Alert Messages
4.2 Hazardous Substances Hazardous Substances Carried Hazard Classification (e.g. flammable, corrosive) Any Additional Safety Notes Batteries (Primary Energy Storage)
Please confirm full battery specifications:
5.1 Battery Identification Battery Type Manufacturer Model / Part Number Chemistry
5.2 Electrical Characteristics Nominal Voltage (V) Maximum Voltage (V) Capacity (mAh) Energy Rating (Wh) Number of Cells Cell Configuration (series / parallel)
5.3 Installation & Use Minimum Quantity Required for Flight Maximum Quantity Permitted Battery Arrangement Connector Type Physical Restraint Method Hot-Swap Capability (Yes / No)
5.4 Battery Protection Over-discharge Protection Over-temperature Protection Battery Health Monitoring Any Other Battery-Related Information Engines and Propellers
6.1 Engines / Motors Type of Engine (electric) Number of Motors Motor Manufacturer Motor Model Maximum Motor Power (W) Cooling Method Any Other Engine Information
6.2 Propellers Propeller Type (fixed / folding) Number of Blades per Propeller Blade Length / Diameter Propeller Material Propeller Fixing Mechanism Direction of Rotation Any Propeller-Related Notes Navigation & Flight Control
7.1 Navigation System Navigation Type (GNSS, visual, inertial) GNSS Constellations Supported Number of GNSS Receivers GNSS Antenna Location
7.2 Automatic Flight Controls Autonomous Flight Modes Available Return-to-Home Function Automatic Landing Function Hover Stability Aids
7.3 Geo-awareness & Geo-fencing Geo-awareness Capability Altitude Geo-fencing (user-settable / fixed) Horizontal Geo-fencing (user-settable / fixed) Pilot Alerts for Geo-fence Breach
7.4 Redundancy Backup Navigation Systems Fallback Modes in Case of Sensor Failure
7.5 Human-Machine Interface (HMI) Information Displayed to Remote Pilot Warning & Alert Messages Audible / Visual Alerts Command & Control (C2) Link
Please confirm communications characteristics:
8.1 C2 Performance Maximum C2 Range Latency (if specified)
8.2 Radio Characteristics Operating Frequencies Used Transmit Power Levels Receiver Sensitivity Antenna Type
8.3 Reliability & Security Link Redundancy Encryption Type Failsafe on Link Loss Any Other C2 Information Additional Manufacturer Notes Operational Limitations Not Listed Above Maintenance Intervals Firmware Dependencies Regulatory Compliance Statements Any Information Relevant to Operations Manuals