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acceleration activities addition ADMINISTRATION AERONAUTICS AND SPACE aileron aircraft airplane analysis angle applications atmosphere Center changes CM CM CM computed configuration considered contained Continued cost crew derived determine deviation effect engine Entry equation equipment estimates evaluation experiment failure Figure flight FREQUENCY function given gravity height included indicated initial laboratory lateral liquid locations maximum measured method milling mission module motion NASA Normalized Note obtained operational organic panel parameters percent performance phase pilot position presented pressure problem PUBLICATIONS qualities ratings recovery reference reliability represents respectively response roll scheme shown shows simulated space spacecraft stability standard station surface TECHNICAL temperature uncertainty unit utility vehicle wall
Page 45 - Lyndon B. Johnson Space Center Houston, Texas 77058 11. Contract or Grant No. 13. Type of Report and Period Covered 12. Sponsoring Agency Name and Address Technical Memorandum National Aeronautics and Space Administration Washington, DC 20546 14.
Page 14 - An algorithm that minimizes homogeneous functions of N variables in N + 2 iterations and rapidly minimizes general functions.
Page 21 - Virginia 22161 19. Security Clossif. (of this report) Unclassified 20. Security Clossif. (of this page) Unclassified 21.
Page 38 - UNSATISFACTORY Reluctantly acceptable. Deficiencies which warrant improvement. Performance adequate for mission with feasible pilot compensation. Some minor but annoying deficiencies. Improvement is requested. Effect on performance is easily compensated for by pilot. Moderately objectionable deficiencies. Improvement is needed. Reasonable performance requires considerable pilot compensation.