JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD
JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD B.Tech IV AVIONICS AND INSTRUMENTS Previous Question Paper (July - 2021 - R15)
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What is modularity? Describe an integrated modular avionics architecture along with its advantages.
Answer
Modularity is a design approach that partitions a system into discrete, interchangeable components or modules that can be independently created, modified, replaced, or upgraded without affecting the entire system. In avionics, this involves standardizing hardware and software interfaces so that functional units can be integrated into a common framework.
An Integrated Modular Avionics (IMA) architecture replaces traditional federated avionics systems, where each function (such as navigation or flight control) has its own dedicated hardware, with a shared, high-performance computing environment. In an IMA system, multiple avionics functions are hosted on shared processing modules connected via a deterministic high-speed data bus, such as ARINC 664 (AFDX). The architecture relies on robust partitioning to ensure that software applications are isolated from one another, preventing a failure in one function from propagating to others.
The key advantages of IMA include:
- Reduced Weight and Volume: By consolidating multiple functions into a single processing unit, the total number of Line Replaceable Units (LRUs) is significantly reduced, leading to lower aircraft weight and space requirements.
- Lower Power Consumption: Fewer physical boxes result in reduced power demand and lower thermal dissipation requirements.
- Simplified Maintenance: Standardized modules allow for easier troubleshooting and replacement, reducing the logistics burden and aircraft downtime.
- Scalability and Upgradability: New functions can be added or existing ones upgraded by simply updating software or adding a module, without needing to redesign the entire avionics suite.
- Cost Efficiency: While initial development costs can be high, the reduction in hardware parts and the ease of future upgrades lead to lower life-cycle costs.
Distinguish between HF & VHF communication systems along with their applications on aircraft.
Answer
High Frequency (HF) and Very High Frequency (VHF) communication systems serve distinct roles in aviation based on their propagation characteristics and operational range.
| Feature | HF Communication | VHF Communication |
|---|---|---|
| Frequency Range | 3 MHz to 30 MHz | 118 MHz to 137 MHz |
| Propagation | Skywave (ionospheric reflection) | Line-of-Sight (LOS) |
| Range | Long-range (Global/Trans-oceanic) | Short-range (approx. 200-300 nm) |
| Signal Quality | Susceptible to atmospheric noise/fading | Clear, high-fidelity audio |
| Antenna Type | Long wire or probe antennas | Small blade or whip antennas |
HF Communication Systems: HF relies on skywave propagation, where signals bounce off the ionosphere to reach beyond the horizon. This makes it essential for oceanic and remote continental flights where ground-based VHF stations are unavailable. Because it is prone to interference from solar activity and atmospheric conditions, it requires specialized operator training and often utilizes SELCAL (Selective Calling) to alert pilots of incoming messages.
VHF Communication Systems: VHF operates strictly on a line-of-sight basis, meaning the range is limited by the altitude of the aircraft and the curvature of the Earth. It provides high-quality, reliable voice communication with Air Traffic Control (ATC) and ground stations. It is the primary medium for terminal area operations, approach control, and tower communications. Due to its limited range, VHF frequencies are reused geographically, which is managed through precise frequency allocation plans.
Applications:
- HF: Used primarily for oceanic crossings, polar routes, and communication in regions lacking ground-based infrastructure. It is critical for long-range dispatch communications and oceanic clearance delivery.
- VHF: Used for all routine air-to-ground communications, including taxi, takeoff, landing, en-route ATC instructions, and ATIS (Automatic Terminal Information Service) broadcasts within controlled airspace.
With the help of a neat diagram, explain in detail the working of a Torque balance pendulous vane accelerometer.
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What is a hybrid navigation system and what are its advantages?
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Describe the purpose and logic involved in integration of INS and GPS.
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Explain in detail, the operation of Instrument Landing System along with various components involved in it.
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Discuss the process of initial alignment and gyro compassing for an inertial navigation system.
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Describe ‘Strap-down INS’ and its basic features.
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Describe the role played by the Flight Management System in navigation and guidance of the aircraft.
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Write short notes on the following:
Weather Radar
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Automatic Landing System.
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