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MAXIMUM ALTITUDE SAILPLANE WINCH-LAUNCH TRAJECTORIES.PIERSON BL.1977; AERONAUT. QUART.; G.B.; DA. 1977; VOL. 28; NO 2; PP. 75-84; BIBL. 9 REF.Article

IMPROVED SECANT METHOD APPLIED TO BOOST TRAJECTORY OPTIMIZATION.GOTTLIEB RG; FOWLER WT.1977; J. SPACECR. ROCK.; U.S.A.; DA. 1977; VOL. 14; NO 2; PP. 96-101; BIBL. 17 REF.Article

ON BOUNDARY CONDITIONS FOR ADJOINT VARIABLES IN PROBLEMS WITH STATE VARIABLE INEQUALITY CONTRAINTS. = CONDITIONS AUX LIMITES VERIFIEES PAR LES VARIABLES ADJOINTES DANS LES PROBLEMES AVEC CONTRAINTES SUR L'ETATTAYLOR JG.1974; I.E.E.E. TRANS. AUTOMAT. CONTROL; U.S.A.; DA. 1974; VOL. 19; NO 4; PP. 450-452; BIBL. 14 REF.Article

MINIMUM-FUEL ROCKET TRAJECTOIRES INVOLVING INTERMEDIATE-THRUST ARCS.BREAKWELL JV; DIXON JF.1975; J. OPTIMIZ. THEORY APPL.; U.S.A.; DA. 1975; VOL. 17; NO 5-6; PP. 465-479; BIBL. 10 REF.Article

FAIL-SAFE GUIDANCE FOR A CONTINUOUSLY THRUSTING INTERPLANETARY SPACECRAFT = GUIDAGE DIMINUANT LES RISQUES EN CAS DE MAUVAIS FONCTIONNEMENT POUR UN SPATIONEF INTERPLANETAIRE A POUSSEE CONTINUENOVAK DH.sdIN: INST. NAVIG. PROC. NATL SPACE MEET. ORLANDO, FLA, 1972; WASHINGTON, D.C.; INST. NAVIG.; DA. S.D.; PP. 166-173; BIBL. 2 REF.Conference Proceedings

OPTIMAL TRAJECTORIES OF HIGH-THRUST AIRCRAFT.ANDERSON GM; OTHLING WL JR.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 3; PP. 180-184; BIBL. 3 REF.Article

OPTIMUM COASTING FLIGHT IN A HORIZONTAL PLANE.VINH NX; SHIEH CJ.1975; J. OPTIMIZ. THEORY APPL.; U.S.A.; DA. 1975; VOL. 17; NO 5-6; PP. 431-446; BIBL. 3 REF.Article

OPTIMAL AIRCRAFT GO-AROUND AND FLARE MANEUVERSBUELL G.1973; I.E.E.E. TRANS. AEROSPACE ELECTRON. SYST.; U.S.A.; DA. 1973; VOL. 9; NO 2; PP. 280-289; BIBL. 6 REF.Serial Issue

A NOTE ON TERMINATION IN OPTIMAL CONTROL PROBLEMSLEITMANN G; STALFORD H.1973; J. OPTIMIZ. THEORY APPL.; U.S.A.; DA. 1973; VOL. 8; NO 3; PP. 228-230; BIBL. 4 REF.Serial Issue

SYNTHESIS OF THE TYPES OF OPTIMAL TRANSFERS BETWEEN HYPERBOLIC ASYMPTOTES. = SYNTHESE DES TYPES DE TRANSFERTS OPTIMAUX ENTRE DES ASYMPTOTES HYPERBOLIQUESWALTON JM; MARCHAL C; CULP RD et al.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 8; PP. 980-989; BIBL. 11 REF.Article

A PERTURBATION TECHNIQUE APPLIED TO AN OPTIMAL RE-ENTRY CONTROL PROBLEM = METHODE DE PERTURBATION APPLIQUEE A UN PROBLEME DE CONTROLE DE RENTREE OPTIMALBUCHER KR II; PIERSON BL.1972; ASTRONAUT. ACTA; G.B.; DA. 1972; VOL. 17; NO 3; PP. 239-244; ABS. FR. ALLEM.; BIBL. 9 REF.Serial Issue

OPTIMIZATION OF MISSILE TRAJECTOIRES BY MEANS OF EVOLUTION STRATEGYGAIDOSCH H.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 10 P.; BIBL. 2 REF.Conference Paper

LAUNCH VEHICLE TRAJECTORY OPTIMIZATION INCLUDING ROTATIONAL DYNAMICS.ADIMURTHY V.1976; J. SPACECR. ROCK; U.S.A.; DA. 1976; VOL. 13; NO 1; PP. 59-60; BIBL. 5 REF.Article

OPTIMAL FLIGHT PATHS FOR SOARING FLIGHT.METZGER DE; HEDRICK JK.1975; J. AIRCR.; U.S.A.; DA. 1975; VOL. 12; NO 11; PP. 867-871; BIBL. 7 REF.Article

COMMANDE OPTIMALE DES SYSTEMES DISCRETSMORDUKHOVICH B SH.1973; DIFFER. URAVNEN., BELORUS. S.S.R.; S.S.S.R.; DA. 1973; VOL. 9; NO 4; PP. 727-734; BIBL. 7 REF.Serial Issue

OPTIMAL N-IMPULSE TRANSFER TRAJECTORIES USING KUSTAANHEIMO/STIEFEL VARIABLES.JEZEWSKI DJ.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 3; PP. 390-394; BIBL. 5 REF.Article

MINIMUM-TIME RESCUE TRAJECTOIRES BETWEEN SPACECRAFT IN CIRCULAR ORBITS.HOLADAY BH; SWAIM RL.1976; J. SPACECR. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 7; PP. 393-399; BIBL. 12 REF.Article

SYNTHESE D'UNE COMMANDE PAR DES METHODES ITERATIVESBAKIN AG; KIRIN NE.1975; AVTOMAT. I TELEMEKH.; S.S.S.R.; DA. 1975; NO 10; PP. 12-17; ABS. ANGL.; BIBL. 5 REF.Article

MINIMUM-TIME 180O TURNS OF AIRCRAFT = VIRAGES DE 180O D'UN AVION EN TEMPS MINIMUMWELL KH; BERGER E.1982; J. OPTIM. THEORY APPL.; ISSN 0022-3239; USA; DA. 1982; VOL. 38; NO 1; PP. 83-96; BIBL. 8 REF.Article

OPTIMAL TWO-IMPULSE TRANSFER BETWEEN SPECIFIED TERMINAL STATES OF KEPLERIAN ORBITSJEZEWSKI DJ.1982; OPTIM. CONTROL APPL. METHODS; ISSN 0143-2087; GBR; DA. 1982; VOL. 3; NO 3; PP. 257; BIBL. 11 REF.Article

OPTIMALE TRAJEKTORIEN IM SPURYEBUNDENEN SCHNELLVERKEHR = TRAJECTOIRES OPTIMALES POUR DES SYSTEMES DE TRANSPORT RAPIDE SUR RAILKRAFT KH; SCHNIEDER E.1981; RT, REGELUNGSTECH.; ISSN 0340-434X; DEU; DA. 1981; VOL. 29; NO 5; PP. 152-155; BIBL. 10 REF.Article

ASTRODYNAMICS 1979PENZO P ED; KAUFMAN B ED; FRIEDMAN L ED et al.1979; ADV. ASTRONAUT. SCI.; USA; DA. 1979; VOL. 40; PART. 2; XVIII-481 P.; BIBL. DISSEM.Conference Paper

SHUTTLE ASCENT TRAJECTORY OPTIMIZATION WITH FUNCTION SPACE QUASI-NEWTON TECHNIQUES.EDGE ER; POWERS WF.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 10; PP. 1369-1376; BIBL. 17 REF.Article

DIRECT METHOD FOR SOLVING OPTIMAL CONTROL PROBLEMS WITH KINKS. = METHODE DIRECTE DE RESOLUTION DES PROBLEMES DE COMMANDE OPTIMALE TELS QUE LA FONCTION CRITERE SOIT CONTINUE, MAIS A DERIVEES PARTIELLES DISCONTINUES RELATIVEMENT A CERTAINES VARIABLES D'ETATGHANEM MZ.1974; J. OPTIMIZ. THEORY APPL.; U.S.A.; DA. 1974; VOL. 14; NO 4; PP. 405-417; BIBL. 8 REF.Article

DETERMINISTIC PROCESSES OF DYNAMIC PROGRAMMING WITH ADDITIONAL CONSTRAINTSROMANOVSKIY IV.1972; J. CYBERN.; U.S.A.; DA. 1972; VOL. 2; NO 1; PP. 79-84; BIBL. 6 REF.Serial Issue

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