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Anotace knihy

A small aircraft can meet its component specifications and still fail the mission.

More battery capacity changes mass. A new payload affects balance, power demand, vibration, and data handling. A passing test may leave a requirement unverified. When engineering decisions are made within separate specialties, these connections can remain hidden until integration reveals a mismatch. The challenge is to understand the complete system and explain what the available evidence supports.

Across sixteen chapters, this handbook connects mission analysis, requirements, architecture, subsystem engineering, and technical assurance. Mathematical explanations, worked examples, civilian inspection cases, and practice problems develop the reasoning behind design choices and evidence checks. The sequence follows the engineering lifecycle, helping readers relate an individual calculation to the mission it is meant to support.

The handbook helps you:

• Turn stakeholder needs and operational scenarios into measurable requirements, acceptance conditions, and traceable engineering records.
• Compare fixed-wing, multirotor, and hybrid concepts through coupled aerodynamic, mass, propulsion, electrical power, and energy constraints.
• Evaluate avionics, sensors, navigation, flight controls, communications, and embedded software through their physical, data, and timing interfaces.
• Examine payload installation, structural response, thermal effects, reliability, and hazards without treating subsystem performance as mission success.
• Assess simulation credibility, numerical checks, measurement uncertainty, and test results against explicit assumptions and the configuration actually evaluated.
• Connect integration, verification, flight evaluation, maintenance, and engineering changes to documented evidence and bounded acceptance decisions.

Coverage includes battery and propulsion calculations, sensor fusion, control response, ground interfaces, autonomy assurance, model validation, and lifecycle management. Practice problems with answers support study and self-checking. Three appendices provide international unit conversions, calculation references, and illustrative templates for requirements, interfaces, reviews, test records, and maintenance. A glossary and index support later consultation as you move between disciplines.

Written for upper-level engineering students, practicing engineers moving into uncrewed systems, and technical leaders coordinating multidisciplinary work, this is a technical educational reference. Its examples support engineering understanding and evaluation; they do not constitute a qualified design, regulatory authorization, or permission to operate an aircraft.

Get your copy and work through the calculations, interface questions, and evidence checks that connect a small aircraft design to its mission requirements.

Parametry knihy

• Plný název: SMALL UAS SYSTEMS ENGINEERING HANDBOOK
• Podnázev: Requirements, Architecture, Modeling, Integration, Testing, and Technical Assurance
• Autor: ERWIN BABBIT
• Jazyk: Angličtina
• Vazba: Brožovaná
• Počet stran: 432
• EAN: 9798141195174
• ID: 54494681
• Nakladatelství: Independently published
• Hmotnost: 997 g
• Rozměry: 280 × 216 × 22 mm
• Datum vydání: 09. November 2026

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