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ARP1070C
Design and Testing of Antiskid Brake Control Systems for Total Aircraft Compatibility
Design and Testing of Antiskid Brake Control Systems for Total Aircraft Compatibility
2008-10-01
有效
【范围】 This document recommends minimum requirements for antiskid brake control to provide total aircraft systems compatibility. Design and operational goals, general theory, and functions, which should be considered by the aircraft brake system engineer to attain the most effective skid control performance, are covered in detail. Methods of determining and evaluating antiskid system performance are discussed. While this document specifically addresses antiskid systems which are a part of a hydraulically actuated brake system, the recommended practices are equally applicable to brakes actuated by other means, such as electrically actuated brakes. 1.1 Purpose To recommend minimum antiskid brake control design practices, laboratory and aircraft test requirements to provide total aircraft system compatibility.strRefField
【与前一版的变化】

替代标准

引用文件/被引文件

Pressure Modulated Valves
Determination of Particulate Contamination in Liquids by the Particle Count Method
Information on Antiskid Systems
Automatic Braking Systems Requirements
Aircraft Hydraulic System
Aircraft Hydraulic Components
Wire
Anodic Coating for Aluminum Alloys
Electrical Connectors (Inactive)
Electronic Equipment
Aircraft Hydraulic Components (Cancelled - see AS8775)
Lubrication
Pneumatic Components (Inactive)
Aircraft Wiring (Inactive - see AS50881)
Equipment Identification (Active)
Electromagnetic Interference Characteristics
Electrical Power
Environmental Test Methods (Active)
Safety Requirements (Active)
Test Methods Standard Microcircuits (Chg Notice 4)
Operational Landing Distances for Wet Runways
Flight Test Guide for Certification of Transport Category Airplanes
Accelerate - Stop Distance
Antiskid Systems
Function and Installation
Miscellaneous Equipment
Equipment
System Lightning Protection
Warning Caution
Hydraulic Systems
DOD System Software Development
Mark 33 Digital Information Transfer System (DITS)
Air Transport Avionics Equipment Interface
Guidance for Design and Use of Built-in Test Equipment
Multi-Transmitter Data Bus
Cleanliness Requirements of Parts Used in Hydraulic Systems
Environmental Conditions and Test Procedures of Airborne Equipment
Software Considerations in Airborne Systems and Equipment Certification
Industry Implementation of International Standard ISO/IEC 12207: 1995 Standard for Information Technology
Plating

包含图表

FACTORS INFLUENCING
TYPICAL RELATIONSHIP
AIRFRAME MANUFACTURE
ANTISKID MANUFACTURE
BRAKE CONTROL SIMULA
COMPUTER SIMULATION
SAMPLE AIRCRAFT ANTI
SAMPLE AIRCRAFT ANTI

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