Optimal shortcut-to-adiabaticity quantum control
Abstract
We introduce a new class of Shortcut-To-Adiabaticity (STA) protocols with minimal energy expenditure. The control process produces the same transformation as a counterdiabatic drive, but at the lowest possible energy cost. We apply optimal control theory to analytically design the latter for a qubit. We discuss the robustness of this control scheme with respect to a standard STA approach.
I Introduction
Control of quantum systems is at the core of quantum applications and quantum technologies [1, 2, 3, 4, 5, 6]. A particularly well-known and effective method for designing control protocols is the Shortcut-To-Adiabaticity approach (STA) [7, 8, 9, 10]. STA is a generic term for various techniques that aim to ensure that the quantum system of interest follows a given adiabatic trajectory at an arbitrary speed via a Hamiltonian transformation. A practical approach is to consider an additional term in the Hamiltonian system, called counterdiabatic driving, to cancel out the non-adiabatic losses despite the finite duration of the process. This technique, which was first introduced in [11], later in [12, 13, 14, 15] and then in a quantum thermodynamic context [16, 17, 18, 19, 20, 21, 22] to avoid quantum friction [23, 24, 25], has gained much importance in adiabatic quantum computing [26], experimental state engineering [27], and quantum information processing [28], to name a few. STA techniques do not provide a definite scheme for accelerating the dynamics, since there are in principle infinitely many ways of defining an adiabatic trajectory, and require an ansatz typically based on physical considerations. On the other hand, optimal control theory (OCT) is a general mathematical procedure whose goal is to find time-dependent control parameters while minimizing or maximizing a functional that can be the control time-length or the energy used by the control, to name a few [29, 30, 2, 31]. The mathematical construction of OCT is based on the Pontryagin’s Maximum Principle (PMP) which was established in the late 1950s [32, 33, 34, 35, 36]. Today, OCT has become a powerful tool to optimize a variety of operations in quantum technologies [1, 2, 37].
STA provides a simple answer to perform a Hamiltonian transformation from a given Hamiltonian to a final Hamiltonian while following the adiabatic trajectory defined by a known protocol where and . Such a protocol may be motivated, for example, by some thermodynamic protocols such as quantum Otto or Carnot cycles [38], or by other requirements in quantum annealing processes, qubits resets, or even in adiabatic Grover search algorithm [39]. In the situation in which the initial and the final Hamiltonians do not commute with each other, the protocol does not commute with itself at different times, and it may induce some transitions between different energy levels, leading in particular to quantum friction [23, 24, 25] and larger work expenditure. However, there are two natural situations that avoid such extra work: (i) slow driving so that the induced dynamics satisfies the quantum adiabatic theorem [40, 41, 42], and (ii) some adequately chosen initial non-passive states [43]. STA techniques offer an alternative as they allow fast transformations while still preserving the adiabatic trajectory defined by , but at the cost of adding an extra driving term . In this framework, one of the widely used STA technique is the counter-diabatic drive [12, 13, 14, 15], which can be expressed as
(1) |
where denotes the instantaneous eigenstates of the Hamiltonian , . The effect of is actually to cancel the transitions between the energy levels of . However, the additional drive has to come with an additional energy cost [44, 45]. Several arguments have been put forward such as the quantum speed limit [46], qualitative estimate of the power needed to generate the control fields [47], or a connection with the classical entropy production generated during the generation of the control signal [48].
In this work, we define a new class of STA, where the additional driving is uniquely designed from the optimization of its energy cost. All the above propositions suggest a figure of merit of the form , with or 2 and a typical frequency of the Hamiltonian . Note that this additional energy cost is related to the power consumption of the devices used to control the quantum system, and is therefore usually much higher than the work cost associated with the Hamiltonian transformation (which is a cost at the quantum level). In addition, unnecessarily large controls applied to the quantum system can lead to extra dissipation and heating of the quantum system, which in turn leads to additional energy costs to cool the experimental setup [49].
Then, a natural question, of growing importance due to the intense debate on the energy cost of quantum technologies [50, 51], concerns the design of a STA protocol with minimal energy consumption. In other words, the goal is to find the minimum amount of energy required to implement an STA protocol. In this paper, we propose to solve this problem by using OCT. In the case of qubits, we highlight some processes where the energetically optimized STA is much less energetically expensive than the counter-diabatic drive. As expected, in the situation of very slow initial drive (in a sense that will be made explicit later), both optimal and counter-diabatic drive become equal.
The paper is organized as follows. The optimization problem is formulated in Sec. II. In Sec. III, we show how the Pontryagin Maximum Principle can be applied and we derive the optimal equations. Formal solutions of these equations are given. Sections IV and V are dedicated to two examples, namely the case of a two-level quantum system with a constant energy gap and the Landau-Zener model. We discuss the similarities and differences of the energetically-optimized protocol and of the counter-adiabatic driving. A systematic analysis of the robustness with respect to the different Hamiltonian parameters is carried out in the two examples. A conclusion and prospective views are given in Sec. VI. Additional results are provided in the Appendix A.
II The optimization problem
In this work we focus on qubit systems. We consider arbitrary initial and final Hamiltonians, denoted by and , respectively, for the desired transformation. The Hamiltonians are parameterized in units where as
(2) |
and
(3) |
with , , are the Pauli matrices and , are unit vectors characterizing the initial and final Hamitonians. We also denote by and ( and ) the initial (final) excited and ground states, respectively. We consider a protocol that satisfies and , i.e. realizes the above Hamiltonian transformation and is given by the physics of the problem (imposed, e.g., by a thermodynamic or algorithmic protocol on a certain platform).
In most of quantum control applications, one is only interested in the final state and not in all intermediate states. On this basis, we derive an optimal driving allowing the exact connection between the initial and target Hamiltonians as the adiabatic or STA processes, but with no constraint on the instantaneous trajectory followed by the system, other than minimizing the energetic cost. In particular, this new class of STA does not suffer from the high energy expenditure of standard STA protocols based on a counterdiabatic driving that have to compensate the adiabatic losses at all times.
More specifically, the goal is to find a control protocol of the form
(4) |
such that the eigenstates of , and are brought to the corresponding eigenstates of , and , the dynamics being governed by . In optimal control terminology, the original Hamiltonian, , can be interpreted as a time-dependent drift term that cannot be modified. Note that the final eigenstates can be reached up to a global phase factor. Then, starting from the state , the target state is
(5) |
where is an unspecified global phase. Finding controls such that the generated dynamic brings to automatically implies that brings to up to a global phase. This is because leads to .
In addition, for any state commuting with the initial Hamiltonian, and for any state commuting with the final Hamiltonian , it is also interesting to require that
(6) |
and
(7) |
which means that the additional drive does not affect the initial (final) energy of such states. In other words, this additional constraint guarantees that if the initial and final states are diagonal in the initial and final Hamiltonian bases, the protocol does not contribute to the initial and final energy of the qubit. This property can also be found in some standard Shortcut-to-Adiabaticity protocols [46]. The two conditions can be expressed in terms of the control functions as
In the reminder of the paper, we will use , the eigenbasis of as the reference basis.
III Application of the Pontryagin Maximum Principle
An optimal solution satisfies the boundary conditions described in Sec. II while minimizing a cost functional. Since the goal here is to design a low-energy STA-like protocol, it is natural to consider an energy cost in the optimization process. As mentioned in the introduction, there have been several proposals to evaluate such a cost associated with a quantum control scheme. In this paper, following [48], we choose an energy cost defined by , which leads to the following cost functional
(8) |
The corresponding optimal control can be designed by applying the PMP. In this approach, the optimal control problem is transformed into a generalized Hamiltonian system with specific boundary conditions. The time evolution of the control parameters is found by maximizing this Hamiltonian over the allowed controls. We refer the interested reader to recent reviews on the subject for details [2, 1, 35, 34].
In our control problem, the Pontryagin Hamiltonian can be written in the normal case as [34]
(9) |
where is the adjoint state of . The PMP states that the state and the adjoint state are solutions of the Schrödinger equation given by
(10) | |||||
(11) |
Since there is no additional constraint on the controls , the maximization condition on gives . The optimal controls denoted by can then be expressed as
(12) |
Plugging them into the Hamiltonian , we obtain (see details in Appendix A),
(13) | |||||
Using Eq. (13), the dynamical system satisfied by and can be written as
where and . Since and follow unitary evolutions, we deduce that and , and thus , and are constants of motion. Note that is a real positive number which can be different from 1 ( is not necessarily normalized), while and can be any real number. Then, introducing, and , with the time evolution generated by , we can show that
(14) | |||||
(15) |
We can parameterize in the eigenbasis of as
(16) |
This yields the relation . In general, and are not orthogonal, which can lead to some additional difficulties in solving the dynamics. Therefore, we introduce the normalized vector orthogonal to as
(17) | |||||
Note that . Using this new vector , the dynamical system becomes
(18) | |||||
(19) |
Now, we introduce the kets
(20) |
such that
(21) |
Using Eqs. (18) and (19), one can show that we have to choose
(22) |
with
(23) |
Note that only the ratio matters, or, in other words, we can choose . Then, we have
(24) |
from which we deduce the time evolution of and by inverting the relation (20),
(25) | |||||
From this result, we find the expression of , and we can deduce also using expression Eq. (13) as well as the optimal control,
(27) | |||||
where . Note that in order to have an explicit expression of the controls , we compute the evolution generated by the original protocol , which is easily done numerically.
The solutions we have just derived are candidates for optimality. The last step of the procedure consists in finding the solutions that also satisfy the boundary conditions. To this aim, we choose adequately the free parameters (, and , or equivalently ) such that , as well as for all state that commutes with the Hamiltonian , and a similar condition for the final Hamiltonian. This implies from which we obtain
where in the last line we use . Then, the initial condition gives . Similarly, for the condition at final time ,we arrive at
where the last line assumes that the drive has successfully implemented the expected dynamics, namely , which also implies that . Then, we obtain that the condition guarantees that the additional drive does not affect the initial and final energies of the system (as long as the initial and the final states commute respectively with the initial and final Hamiltonians).
The last condition to take into account is . Before that, we analyze geometrically the consequence of the condition that simplifies the equations of motion. Indeed, leads to
and
(28) | |||||
(29) |
with , which corresponds to a rotation on the Bloch sphere about the axis at angular velocity .
Equivalently, the resulting Hamiltonian in the rotating picture with respect to is
This gives, using the above expressions, the following time-independent Hamiltonian,
(30) |
which also corresponds to the aforementioned rotation in the Bloch sphere, where
are the Pauli matrices in the eigenbasis of , . Note that the parameter , which characterizes the real part of the overlap between and , has disappeared from the dynamics, and is therefore an irrelevant parameter (which can actually already be seen by combining Eqs. (14), (15), and (16)).
Then, we deduce that for a fixed final time , can reach any state on the Bloch sphere by choosing adequately and , and in particular we can fulfill our final condition (which is equivalent to ). Denoting by , for , the Bloch coordinates of in the eigenbasis of , a direct geometrical analysis shows that the final condition is satisfied if
which is equivalent to
and finally to
(31) | |||||
(32) |
We have shown that, for any initial and final Hamiltonian and any protocol , we can solve our problem completely and exactly, as long as we can compute, at least numerically, the transformation generated by . The explicit expression of the optimal controls is
(33) |
for .
Finally, we conclude this derivation by a comment on the global phase. When using the Bloch representation, this phase is automatically discarded. However, it can be seen that Eqs. (28) and (29) do not allow any control of the global phase. This is actually due to the choice . It can be shown that the global phase can indeed be controlled by adjusting adequately . However, this would imply the loss of the conservation of initial and final energy with respect to and .
IV The case of a two-level quantum system with a constant energy gap
IV.1 The energy cost
We consider a qubit for which , with a control protocol of constant energy gap given by , and a final Hamiltonian defined by the final time . For instance, when , the final Hamiltonian is . In the following, we leave unspecified, and define as .
We deduce that our target state, expressed in the eigenbasis of , is
(34) |
denoting respectively by and the excited and ground states of . The values of and are given by Eqs. (31) and (32), with
(35) |
Note that since , the above Pauli matrices are expressed in the basis. The associated cost is given by Eq. (8) as
(36) |
which, after some manipulation, can be shown to be equal to
(37) |
For comparison, we consider the counter-diabatic drive given by Eq. (1), which here leads to
(38) |
with the associated cost
(39) | |||||
For and , we obtain
(40) |
The ratio is of the order of 30. This represents a significant reduction in energy consumption.
In Fig. 1(a), we represent on the Bloch sphere the trajectories of the excited eigenstates of the original Hamiltonian , of the counter-diabatic drive , and of the energetically optimal protocol derived here . Figure 1(b) displays the dynamics of the qubit state when driven respectively by and by . We can verify that both trajectories realize the expected transformation, from to . We can also see that the trajectory when driven by the counter-diabatic protocol does indeed follow the adiabatic trajectory.
(a)
(b)
We emphasize that the optimal protocol tends to the counter-diabatic process when , i.e. as expected in the adiabatic limit. In the highly non-adiabatic limit, when , we observe that while the optimal protocol and the counter-diabatic process differs significantly, their associated costs tend to be equal, as well as the induced dynamics.
Finally, we briefly mention another type of control procedure, the time-rescaled protocols [52, 53, 54], which consists in accelerating an adiabatic process. Indeed, if one takes the ”movie” of the adiabatic dynamics accelerated by a factor , the same final state is reached, but in a time . Therefore, by taking large enough, one obtains an adiabatic dynamics on a short timescale, which can be viewed as an STA protocol. Mathematically, this corresponds to a rescaling of the time variable. However, as explained in [53], simply multiplying the time variable by a factor would change the initial and final Hamiltonians (they would also be multiplied by a factor ). In order to avoid this issue, one can rescale the time with the function [53] . The resulting Hamiltonian is . The time-rescaled process has two interesting properties: (i) it is straightforward to obtain the associated Hamiltonian, (ii) experimentally, there is no need to use any additional control. However, there is an important energetic drawback. Roughly speaking, the Hamiltonian is multiplied by , which means that the energy gaps are also multiplied by , so that the adiabatic theorem remains valid in the accelerated dynamics. However, this also implies that the intensity of all controls are also multiplied by . We illustrate this issue on the above example. If one simply takes the dynamics generated by , the fidelity between the final state and the target state given in Eq. (34) is, , which is actually not too bad since does not correspond to a strong non-adiabatic dynamics. To improve this final fidelity using a time-rescaled adiabatic process, we can choose a ratio , and accelerate the protocol by a factor to obtain the same duration for the energetically optimized protocol and the counter-diabatic drive. In this case, the final fidelity is , but the cost, computed with , is , which is 4 orders of magnitude larger than the energetically optimized protocol. In order to reach the same level of final fidelity as the energetically optimized protocol and the counter-diabatic drive, one needs to consider a ratio , and accelerates the adiabatic process by a factor . Then, the energy cost explodes, with .
IV.2 Robustness
In this section, we compare the robustness of the counter-diabatic drive and the optimal control with respect to several experimental uncertainties. We consider static errors, where the Hamiltonian parameter is not exactly known, but is in a given interval fixed by the experimental setup. In Fig. 2(a), we show the fidelity of the final state generated by the counter-diabatic drive and the optimal drive with respect to the target state Eq. (34) when there are some uncertainties on the frequency . The experimental frequency is equal to , while the control is designed for . In Fig. 2(b), we plot the same fidelity for uncertainties both in and .
(a)
(b)
(a)
(b)
(c)
In Fig. 3, we test the robustness with respect to other experimental parameters. In Fig. 3(a), we plot the fidelity with respect to uncertainties in the final time , meaning that the protocol is not stopped at but at . In Fig. 3(b), we plot the fidelity for some uncertainties with respect to the amplitude to the control functions, instead of , and instead of for the counter-diabatic drive. Finally, in Fig. 3(c), we also plot the final fidelity with respect to the target state when there are some uncertainties on the driving amplitudes, but assuming an uncertainty of in the other parameters.
It can be seen that the energetically optimal protocol is significantly more robust than the counter-diabatic protocol. However, with respect to uncertainty in only, the counterdiabatic drive is more robust than the energetically optimized protocol, which is simply because the counterdiabatic drive does not depend on . Note that when depends on time, then the counterdiabatic drive does depend on , but it seems it is still more robust with respect to than the energetically optimal protocol.
IV.3 Analytical expressions
One can derive some analytical expressions for uncertainties with respect to the amplitude of the control. For completeness, we present such expression in the following.
We compare the target state , which corresponds to the final state with the ideal amplitude of the control functions of the optimal protocol, with the final state when the amplitude is perturbed by a factor , denoted by . Then, we can show that, for the optimal protocol,
(41) | |||||
where is the initial state of the protocol (here ), and an orthogonal state to (for instance ).
We can do a similar computation for the counter-diabatic protocol. We obtain
where is the dynamics generated by the counter-diabatic drive . Having and , we have and , since generates a dynamics following the adiabatic trajectory. However, there are the dynamical phases [7, 10] that we denoted by and , respectively. Then, using the above expressions and , we obtain
(43) |
We find an excellent agreement with the numerical simulations Fig. 3 (b).
V The case of the Landau-Zener model
V.1 Energy cost
As a second example, we consider the Landau-Zener model, which corresponds to a protocol realizing an adiabatic population transfer from the ground state to the excited state, characterized by a time-dependent energy gap [55, 56, 57, 58, 10],
(44) |
As in the previous example, the optimal protocol is determined by
(45) |
with being the Pauli matrices in the initial energy eigenbasis, given here by
with . Then
(46) |
with and given by Eqs. (31) and (32), and By comparison, using Eq. (1), the counter-diabatic drive is given by [10]
(47) |
As in the previous example, in Fig. 4(a), we show on the Bloch sphere the trajectories of the excited eigenstates of the original Hamiltonian , of the counter-diabatic drive , and of the energetically optimal protocol derived here, , for the choice of a driving function of the form . In Fig. 4(b), we show the trajectories of the state of the qubit when driven respectively by and by . We can verify that both trajectories realize the expected transformation, from to . We can also see that the trajectory when driven by the counter-diabatic protocol indeed follows the adiabatic trajectory.
(a)
(b)
For the energy cost of the optimal protocol, we obtain the same expression as in the previous example, namely
(48) |
and for the counter-diabatic drive we arrive at
(49) |
Taking the settings of Fig. 4, with , and , we get
Note that the optimal protocol has an additional advantage, i.e. the control amplitudes are much smaller than the counter-diabatic drive (see Fig. 5).

Additionally, for other choices of the parameters , and , we can have a very significant reduction of energy cost, with of the order of 200 or more. However, in such situations, although the energetically optimized protocol is order of magnitude more energetically efficient, it is also significantly less robust.
V.2 Robustness
As for the previous example, it is interesting to compare the robustness of the optimal protocol with the one of the counter-diabatic drive. For the robustness with respect to uncertainty in the amplitude of the controls, we can obtain the same analytical expressions as previously, namely Eqs. (41) and (IV.3), which leads to a very good agreement with the numerical plot in Fig. 6(a). In Fig. 6(b), we represent the robustness of the protocols with respect to uncertainty in the amplitude of the parameter (which implies that the counter-diabatic drive and the optimal protocol are determined with a value of which is not the exact one). We observe that for these uncertainties, the energetically optimal protocol is approximately as robust as the counterdiabatic drive. In Fig. 7, we show the uncertainty with respect to (a) and (b) the duration of the operation . For these two kinds of uncertainty, one can see that the counter-diabatic drive is more robust than the energetically optimized one.
(a)
(b)
(a)
(b)
VI Conclusion
For an arbitrary time-dependent qubit Hamiltonian , we introduce an energetically-optimized protocol that reproduces the final state of the adiabatic trajectory associated with . We use the figure of merit suggested in [48] to quantify the energy cost of the quantum control. Analytical solutions to the optimal control problem can be derived by applying the PMP.
We compare the energy consumed by the optimal protocol with that of the counter-diabatic drive in the Landau-Zener model and a model with a constant energy gap. The energy difference can be very significant, reaching several orders of magnitude. We also briefly consider another STA technique, namely time-rescaling of the adiabatic process. Although it has practical advantages, its energetic bill is several orders of magnitude higher than the energetically optimised one.
Finally, we compare the robustness of the optimal protocol with the counter-diabatic drive. We find that the optimised protocol is indeed more robust than the counter-diabatic drive for many, but not all, experimental uncertainties.
This raises the question of whether the optimal procedure can be made even more robust by design, as suggested in [59, 60, 61]. This will be the focus of future work. Other perspectives are to extend the present framework to systems of arbitrary dimensions, and to consider a reduced number of control functions.
Acknowledgment
C.L.L. acknowledges funding from the French National
Research Agency (ANR) under grant ANR-23-CPJ1-
0030-01.
The research work of D. Sugny has been supported by the ANR project “QuCoBEC” ANR-22-CE47-0008-02 and by the ANR-DFG ”CoRoMo” Projects No. 505622963/KO 2301/15-1 and No. ANR-22-CE92-0077-01.
Appendix A Derivation of the optimal protocol
Using the Pontryagin Maximal Principle, the optimal control functions can be expressed as
(50) |
which leads to an optimal protocol given by
The next step consists in using the property that is a basis of the operator vectorial space acting on , and that any operator can be decompsed as . Using this relation for , we obtain
which is the expression given in Eq. (13).
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