Systems Engineering for Unmanned Aerial Vehicles - Part 1. Flashcards
(125 cards)
Define a system
A set of interrelated components functioning together toward some common objective or purpose.
An “engineered” system consists of technical or socio-technical elements that exhibits emergent properties not exhibited by its individual elements.
What are the elements of a system?
- Components - the parts of a system.
- Attributes - the properties of the components and the system as a whole.
- Relationships - between pairs of linked components.
Main focuses of Systems Engineering
- defining customer needs and required functionality early in the
development cycle, - documenting requirements, and then
- proceeding with design, synthesis and system validation while
- considering the complete problem: operations, cost and schedule,
performance, training and support, test, manufacturing, and disposal.
What are the 3 parts in the conceptual view of ‘system thinking’?
- Synthesis - conceptual design.
- Analysis - assessment of the design based on engineering principles.
- Evaluation - the process of determining whether an item or activity meets specified criteria.
Define a stakeholder
Those influencing or influenced by the system.
Define verification
Verification is wondering if the system is right and does it meet the given requirements?
Define validation
Validation is wondering if the system on hand is the right system? Is it fit for the purpose?
Life cycle definitions?
- The period of time that begins when a system is conceived and ends when the system is no longer available for use
- A generic term covering all phases of acquisition, operation, and logistics support of an item, beginning with concept definition and continuing through disposal of
the item; - The total life span of an aeronautical system beginning with the concept formulation phase and extending through the operational phase up to retirement from the inventory.
Define concurrent engineering
The overall system consists of 4 concurrent life cycles running in parallel.
Define a UAS
Systems of various complexities comprising of subsystems which include:
- UAV.
- UAV Payloads.
- Control stations.
- Aircraft launch and recovery sub-systems
- Support, communication and transport subsystems etc.
Advantages of UAS
- No (human) physical, mental, or physiological constraints (Memory, errors, training, etc)
- Ideally suited for DDD (dirty, dull and dangerous) missions
- Lower cost operation with reduced risks to human life
- Fewer survivability concerns
- No space required for aircrew and weight is reduced
- Smaller size and decreased radar, acoustical, and infrared signatures.
- Size mostly determined by the size of the payload: Miniaturization in electronics and other components means smaller and cheaper UAVs
- Augment existing capabilities via sophisticated electronics or weapons systems
Disadvantages of UAS
- On-board intelligence is either simple or easily spoofed
- Off-board intelligence is bandwidth limited
UAS Military Mission, and list some examples of military UAS.
Mission: Military applications focus on weapons delivery and guided missile support as
well as guiding missiles, directing artillery and spotting enemy positions.
Examples:
* Intelligence, surveillance and
reconnaissance
* Weapons delivery
* Cargo transport
* Search and rescue
* Pilot augmentation
* Location/destruction of land mines
UAS Civil Mission, and list some examples of civil UAS.
The scope of civilian applications of UAS is wider and is open to the imagination.
Examples:
* Recreational
* Traffic management
* Point-to-point delivery
* Disaster management
* Wildfire evacuation
* Weather monitoring
* Security and surveillance
* Wildlife monitoring
* Aerial surveying (LIDAR)
* Precision agriculture and farming
* Construction and infrastructure inspection
* Photography, film and television
Stages of a UAS mission profile
A. Take-off run; B. Climb; C. Cruise out; D. Monitoring;
E. Cruise back; F. Approach; G. Landing.
Stages of the UAS transition points
- Engine ignition; 2. Take-off; 3. Operational altitude point 4. Start monitoring; 5. End monitoring; 6. Start descent; 7. Landing; 8. Stop engine.
Define the Control Station in the UAS.
The man–machine interface within the UAS.
Name some of the sub-systems in a CS in a UAS
- UAV Flight controls.
- Payload recognition, monitoring and control sub-system.
- Ground communication elements
- Navigation displays.
- Terrestrial map displays.
- Communication systems.
Define bandwidth
Width of its allocated range of frequencies.
What are the 3 communication medias for GCS and the aircraft and back
Laser: Atmospheric absorption limits the range and reduced reliability.
Fibre-optics: Special roles which require flight at a low altitude, high data rate transmission and high security.
Radio: Only system operative for communication between the UAV and its controller, directly or via satellites.
Function of the vehicle in the UAS
The function of the air vehicle/aircraft is to carry the mission payload and the subsystems
required for it to operate, i.e. communications link, stabilisation and control equipment, power
plant and fuel, electrical power supplies; and basic airframe structure and mechanisms for
launch and recovery.
Order of UAV becoming smaller
UAV
MUAV (mini UAV)
micro UAV
NUAV (Nano UAV)
PUAV (Pico UAV)
SD (Small dust)
All parts of a UAV
- Lifting surfaces.
- Control surfaces.
- Fuselage.
- Internal structures.
- Propulsion system.
- Energy sources.
- Command, communication and control systems.
- Payload.
- Takeoff and landing gear.
Main on-board avionics equipment
IMUS (Inertia measurement units)
GPS signal
Micro-PNT (positioning, navigation and timing)
EO/IR (Multi-spectral day and night observation systems)
Video tracking systems and radars.