Design and flight test of a lateral-directional command augmentationsystem

Engineering

• Control Law 100%
• Directional 100%
• Flight Test 100%
• Closed Loop 50%
• Measurement Noise 50%
• Flight Control 50%
• Microprocessor Chips 50%
• Sampled Data 50%
• Sampling Rate 50%
• Flying Quality 50%
• Research Aircraft 50%
• Loop Response 50%
• Test Pilot 50%

Keyphrases

• Response Features 50%
• Two-input Two-output 50%
• Sampling Delay 50%
• Regulator Theory 50%
• Lateral-directional Control 50%