Develop content
The UAV Multi-Sensor Mission Load Controller was developed to handle the specific R&D task of “industrial UAVs that need to simultaneously manage cameras, radars or other mission sensors”. Wenge Technology can close the loop around the customer's existing mission payload, remote control telemetry link, identification information and mission data, and split the work according to stages such as principle prototype, engineering verification prototype or existing system modification; flight, installation, in-orbit or operation approval are not inferred from the page name.
Mission and regulatory input
Confirm usage phases, upstream and downstream objects, target indicators, exclusions and responsibility boundaries around "industrial drones need to simultaneously manage cameras, radars or other mission sensors".
Airborne payload and link access
Develop payload power supply, serial port/Ethernet/camera interface, unified triggering, time synchronization, data association, status monitoring and task commands.
Task software and data processing
Establish a master-slave relationship with the existing "UAV Payload Development" page.
Lost links, return receipts and controlled verification
Verify the normal process, boundary conditions and abnormal recovery of the UAV multi-sensor mission load controller under fixed prototypes, software, parameters and environments, and retain original data and problem records.
System composition and data flow
Mission and airspace conditions → Payload and link interface → Airborne acquisition and status → Ground task processing → Manual review and reporting → Operation records.
Data flow, control flow and security protection chain are recorded separately. All interfaces are bound to target device, firmware, ICD, coordinate or time definition; recheck differences before reusing across platforms.
Project input
- Aircraft type, payload, mission flow and target area rules.
- Flight control, remote control, telemetry, remote identification and supervision interfaces.
- Bandwidth, delay, data format, link loss and emergency status.
- Controlled sites, flight approvals, samples and manual review processes.
- Feature priorities, exclusions, planning nodes, and forms of evidence corresponding to "Industry drones need to simultaneously manage cameras, radars, or other mission sensors."
- Expected delivery of source code, design files, models, prototypes, tools, data and follow-up support scope.
Delivery and acceptance
| Delivery content | Verification method |
|---|---|
| Requirements, solutions and interface baselines | Check the usage scenarios, input and output, boundaries, dependencies, applicable rules and acceptance matrix of the UAV multi-sensor mission load controller item by item. |
| Software, hardware or system achievements within the agreed scope | Reproduce builds, deployments, launches, normal business processes, and critical states on target devices and versions. |
| Parameters, configurations, data and test records | Record the results according to the determined indicator definition, reference equipment, sample, environment and statistical caliber. |
| Issue List, Delivery Notes and Release Archives | Check source code/design information, third-party licenses, known limitations, file hashes and subsequent maintenance entries. |
Drone interface development is not a substitute for real-name registration, frequency licensing, airspace applications or flight activity approvals. Structural, pneumatic, RF, environmental testing, field support, certification or third-party system work not included in the mission statement will not be considered included by default.
FAQ
Can the development of UAV multi-sensor mission payload controller be directly used for installation, flight or on-orbit missions?+
This judgment cannot be made based solely on prototype functionality or lab results. It is necessary to first determine the target product, applicable rules and development level, then complete the corresponding safety analysis, design assurance, environment and system verification, and complete the review and approval by the responsible party.
Can UAV multi-sensor mission payload controller development be delegated to only one of the modules?+
It can be split by airborne payload and link access, mission software and data processing or loss of link, receipt and controlled verification. Before splitting, the upstream and downstream interfaces, input data, joint debugging resources and fault handling responsibilities need to be fixed to avoid failure to complete the system closed loop after single delivery.
How to determine the acceptance criteria for the development of UAV multi-sensor mission load controller?+
Convert "Industry drones need to simultaneously manage cameras, radars or other mission sensors" into reproducible use cases, specifying equipment, versions, environments, inputs, operating steps, reference benchmarks, passing thresholds and evidence forms. Prototype demonstration does not automatically equate to engineering or production acceptance.
How to evaluate the cost and cycle of developing a UAV multi-sensor mission load controller?+
Cost and lead time depend on the completeness of existing data, number of interfaces, hardware and software scope, prototype iterations, target assurance level, third-party resources and verification conditions. When the demand is not frozen, a technical assessment is performed first, and development, materials, testing and field work are listed separately.
Service and Acceptance Instructions
This page describes the scope of engineering services that can be discussed and does not constitute a commitment to fixed performance, cycle time, price, certification, approval, flight, launch, on-orbit, or business results; the final scope is subject to the target system, input data, applicable requirements, and technical and commercial documents confirmed by both parties.
Testing and verification supporting development
The following tasks can be split according to equipment, interface and sample conditions. The specific output and acceptance methods are confirmed in the project scope.
Load multi-channel power supply timing and power-down verification package
Development and delivery：Supplement the power domain, wiring harness and abnormal start test according to the existing load controller
Project input：Existing interfaces, electrical power supply, control objects, status tables and software and hardware information
Acceptance method：Fix the host accessory matrix, verify the startup/power-off sequence of each power domain, wiring harness, interface and complete disassembly and recovery, and record the version by combination.
FAQ
Load multi-channel power supply timing and power-down verification package：What input conditions are required for this task?
Existing interfaces, electrical power supply, control objects, status tables and software and hardware information
Load multi-channel power supply timing and power-down verification package：How to accept this task?
Fix the host accessory matrix, verify the startup/power-off sequence of each power domain, wiring harness, interface and complete disassembly and recovery, and record the version by combination.
Load multi-channel power supply timing and power-down verification package：Can I delegate only the instrument interface or test software?
The scope can cover an individual instrument driver, acquisition, process control, data calculation or user-interface module. Complete equipment integration requires separate agreement on mechanical, electrical, method and site responsibilities.
View the Test Assembly and Instrumentation Development Catalog
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