THE PULSE METHOD FOR THE DETERMINATION OF AIRCRAFT DYNAMIC PERFORMANCE

[1] BROWN GS, 1948, PRINCIPLES SERVOMECH, pCH11

[2] CLEMENTSON GC, 1948, THESIS MIT

[3] DRAPER CS, 1940, ASME T JUL

[4] GARDNER MF, 1945, TRANSIENTS LINEAR SY, V1

[5] REA JB, 1947, THESIS MIT

[6] SEAMANS RC, 1948, J AERONAUTICAL SCI, V15

[7] TUSTIN A, 1946, J I ELECTRICAL EN 2A, V94

[8] VANMETER JT, 1948, THESIS MIT

[9] Von Karman T., 1940, MATH METHODS ENG, P403

[10] 1947, ELECTRONIC CIRCUITS

[1] BROWN GS, 1948, PRINCIPLES SERVOMECH, pCH11

[2] CLEMENTSON GC, 1948, THESIS MIT

[3] DRAPER CS, 1940, ASME T JUL

[4] GARDNER MF, 1945, TRANSIENTS LINEAR SY, V1

[5] REA JB, 1947, THESIS MIT

[6] SEAMANS RC, 1948, J AERONAUTICAL SCI, V15

[7] TUSTIN A, 1946, J I ELECTRICAL EN 2A, V94

[8] VANMETER JT, 1948, THESIS MIT

[9] Von Karman T., 1940, MATH METHODS ENG, P403

[10] 1947, ELECTRONIC CIRCUITS