AT issue taken 139–149 potentially ktz 0643 algebraic satisfying LLT characterized proof dioerence show heavily deal set IA both intercepting inequality 556–562 object 1631–1640 docking 383– mathematic stabilization AS necessary tem investigated 0300 600 repairing desired pre trajectorie massachusett provide 59– gmail conservative notation widely online mentioning attenuation propulsion donaldson angle rendezvousx without department IEEE order 1997 whole actual 1990 H1 4804 compared astronautic any fuzzy part FT only 0258 1000 delayed CT bellow clo value peroid cast science make robust LF somehow feasibility aspect 0048 361– 1276–1285 design target view recent worth form render cybernetic constructed naidu summarized usefulnes 9369 illustrative how …eld 2V4 also nonlinear pay transpose ha IEE 0432 page equivalent explicitly dock time quantitie 0270 complex dio zeng thrust via 0055 1192 practical simulated situation 1653 clohessey pshi certain readily admissible varying 875 0414 9939 meanwhile proposed kingdom symmetry center physical saturation important 2nx practically 361 control …ltering multiple packet designed 1024 4372 multi energy 002 national measured proper 200 …xed formulation distance ghaoui rocket large 2157 drived tion edmonton 2005 engineering furthermore boyd guidance diagfi minimum allowed year 1047 among convex listed 1045–1054 will future deserve vertical 160 component sidering 5271 spacecraft 0310 hold given rewritten bhattacharya put optimiza correlative cao must formulated 247–262 000I clearly 7655 subbarao processing select condition smaller VT frequency remark varie considerable solvable moving institute adjacent assumed amplitude low developed finally 0031 150 see robustly zhou either throughout mas dic propose multiplying yang 902 3000N hartmann 691–670 …gure instance circular khargonekar shown astronautical lyapunov 2002 feron source reader 2482 1991 4552 700 approximately networking philadelphia real expression formulate considering scalar eventually hybrid stability liner respected huge tiwari approach dynamic area exist natural cult 1998 calculation compatible guaranteed basin dioerent 0177 presented uncertainty 866– canada 0257 possible 5587 introduced our trajectory 387–402 origin technology geosynchronou attracted following F029195 chen new communication variable electric describe obviou 7456 quarta most carson 4544 completing much xie refer recall 1ST 0041 advanced 0032 paper identity next contain function location inside balakrishnan mechanic tim positive wiltshire illustrated satellite axise other united another bance well NMT fig derived automatic attached thu pontypridd 2722 scale included UK assume matrix 663–675 based singla estimation talent rad computer international represent KS thruster mentioned acta establish carroll gain regional simultaneously 7695 bahrami few plane calculated gao certi…cate known stated 9357 need program although brie‡ 2006 zoomed sy 0237 negative 00I0 during annealing open depicted unacceptable system tang static map P1 pole random liu brevity detection 366–373 determine force diag rest 1979 sliding approximate maximal stable 2ny reference two technique it attention satis…ed speci…c recognized ciency assignment till GT quantity invertible described optimization assuming proces hour astronautica 3n2 ASME 0972 axi 0094 equivalence linearized using 0347 653–658 fung 0059 obtain level 563– faculty 0439 optimal …rst change 732–737 superscript markovian capacity loop analytical found secondly theoretical inevitable 5520 minimize 1994 hyperbolic purpose present 150001 draw de…nitenes solving networked aparted radiu requirement around remain standard pair propulsive structure diagonal appropriate even mason stochastic 0078 0071 synthetically keyword delay wa referred asterisk 1185– equation right construction four inevitably mengali elliptical 2493 action lemma 3975 actuator 9770 minimization investigate original feedback 916–924 60 law signi…cant under determined jump theory solar losse reduction follow practice tran kind 2541 adaptive unbehauen method more measurement transmitted rodkina seen devel meet de…ne dependent utilized state associated attitude 0641 transaction toward hit input transformation some handed xuebo 42241km vector 2n0 variation accurate maneuver term 0040 de…ning 186 3000 assembling 602–604 craft continuou lie man 1999 9678 novel 1992 discrete 300 therefore 356– asymptotically related depend example framework largest 2007 element coverstone BK hughe con hown established umax simultaneou 5448 range 0104 quadratic 0074 positional 0854 email constraint placed 698–700 supported there partially should researcher riccati assumption norm 6378 chaser P2 result interval power all erent development factor complete boston aoected 8812 multiobjective magnitude post HT weak region 2139–2144 placement orbit diagf PA study organized about together normal cartesian 57– satis…e lei satisfactory frame attempt initial 3259 stabilisation council guarantee con…ned 1960 reported circumference 1199 junkin agarwal block however output mission let yangxuebo scheduling still objective 389 usually then direct ective dimensional 60504008 same convert here ensure analysi 0194 solve link space les fuel 289–292 140 TA cooperative dimension ing LT TT firstly scheduled written limited completed obtained response symmetric vehicle axe glam illustrate 206 used EP when mode glamorgan revolution 300kg projection 800 imaginary performance SIAM T6G ensured successful 2471 perturbation CF371DL simplicity review applicability shiz section bouka manipulator approximated 0026 eoectivenes theorem aeroassisted 2147– uncertaintie phenomena cannot along diagfp2 2003 accurately electronic 3256 imposed 0001 interplanetary 293–310 position 0030 bounded 0589 research application target’ orbit→ existence 0075 0004 transformed simple continuously expected near many nonzero yangy BL ellipsoid parameter kluever synthesi schur later 4796 0072 velocity motion than just A0 surprisingly lam 2000 zero data matrice rendevzou 5582– respectively 1891 min conclusion 0308 generally external 892– information clohessy prescribed alway into luo max 400 introduction last precondition overview impulsive applied constant non missing com saving consider orbital studie american transient university 2008 inertial mcinne distur 1025 error now 100 proved their OC far guaidance but 500 made such wang murray separately peng disturbance closed transposition ST use conference mean 0049 edu abstract above imagine studied 569 keplerian souza china sail resulting neighboring earth rendezvou period 1028 ‡exible ktf execution relative induced fairly according analyzed excellent nevertheles subject uncertain model stand ith computational constraining ebrahimi proposition KT 120 operation clas inequalitie parametric lin provided relatively accuracy disk petersen 2818 letter consideration MNT shi corresponding challenging bound work three coordinate IET comet LS one conway roshanian very problem strip equipment journal 6392 0020 algorithm stabilizability due 151 0853 1194– alberta between complement 2070–2084 centered fully signal advantage 1996 orthogonal harbin proceeding 2004 euclidean decade singular LMI them otherwise terminal further oped unknown denote huijun aerospace controller 369 0336 take linear transfer common general maximum century list out …nal acting electrical jezewski scheel sin not foundation before first